Open-air traveling-wave thermoacoustic generator

Size: px
Start display at page:

Download "Open-air traveling-wave thermoacoustic generator"

Transcription

1 rticle Engineering Thermohysics July 11 Vol.56 No.: doi: 1.17/s x SPECIL TOPICS: Oen-air traeling-wae thermoacoustic generator XIE XiuJuan 1*, GO Gang 1,, ZHOU Gang 1 & LI Qing 1 1 Key Laboratory of Cryogenics, Technical Institute of Physics and Chemistry, Chinese cademy of Sciences, Beijing 119, China; Graduate Uniersity of Chinese cademy of Sciences, Beijing 149, China Receied Noember 19, 1; acceted February 15, 11 Taking the inut and reflected waes into account, the relationshi between the acoustic imedance at the end and the inut of a system were theoretically analyzed. Closed and oen acoustic configurations that influence the ressure, olumetric elocity, imedance and acoustic work were comared in detail. Based on the aboe inestigation, an oen-air traeling-wae thermoacoustic generator was designed and fabricated. It is comosed of a looed tube, a resonator oen at one end, a regenerator, and hot and cold heat exchangers. It is a small scale and simle configuration. The resonant frequency is 74 Hz at 1 bar in air. The maximum acoustic ressures at the oen end and.5 m far away from the oen end are db and 11 db from a reference alue of μpa when the heating ower was 1 W, resectiely. coustic ressure is reasonable for ractical alication as a low-frequency acoustic source. In further work, we beliee that the acoustic ressure at the oen end can achiee 15 db, which could be a solution to roblems in existing acoustic generators. These roblems include low acoustic ressure and system comlexity. It can be used as a basic acoustic source for low frequency and long-range noise exeriments, and as a suly for high acoustic ressures necessary for industrial sources. oen-air, traeling-wae, thermoacoustic generator Citation: Xie X J, Gao G, Zhou G, et al. Oen-air traeling-wae thermoacoustic generator. Chinese Sci Bull, 11, 56: , doi: 1.17/s x The thermoacoustic rincile [1] is a thermodynamic effect that occurs between comressible gases (the first medium) and solids (the second medium) in an acoustic field. It results in a time-aeraged heat flow and a time-aeraged work flow along (against) the sound roagation direction at enetration deths that are far from the solid boundaries. The conersion of heat to work is called thermal to acoustic effect, and the oosing rocess is called the acoustic to thermal effect. Based on these two effects, thermoacoustic systems can be classified as thermoacoustic engines and thermoacoustic refrigerators. regenerator in an acoustic field can bring standing-waes [,3], traeling-waes [4 6] and standing traeling waes [7,8] into being. In the latest two decades, engineering alications in thermoacoustic refrigeration and thermoacoustic electricity hae been raidly deeloed. In 199, thermoacoustic engines first re- *Corresonding author ( xiexiujuan@mail.ic.ac.cn) laced linear comressors to drie ulse tube refrigerators [9]. Researchers of China hae focused on large-scale thermoacoustic engines to drie ulse tube refrigerators and high-frequency thermoacoustic systems since [1 1]. Recently, a new lowest cooling temerature in liquid hydrogen, K, was achieed [13]. In 3, the thermoacoustic engine was alied in an electrical field to drie a linear C generator [14]. Luo s grous [15] inestigated thermoacoustic electricity rototyes and linear generators, which is caable of roducing electric owers in the hundreds of watts. For acoustic configurations, thermoacoustic comonents such as regenerators and heat exchangers can be inserted into a closed resonator to create many tyes of thermoacoustic engines. The closed configuration can be filled with gases at MPa mean ressures. The gas tyes that can be used are flexible, including nitrogen, helium, argon, and a He-r mixture. The highest mean ressure that has been The uthor(s) 11. This article is ublished with oen access at Sringerlink.com csb.scichina.com

2 168 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. used is 5.5 MPa [14]. Howeer, only thermoacoustic comonents that can withstand these ressures can be used. Thermoacoustic owers generally scale with m a, which is a dimensionless reference. Hence, for a gien ressure ratio 1 / m, a high mean ressure and high acoustic seed of gases yield a high ower er unit olume of the system. Light gases also hae a high thermal conductiity, which leads to higher enetration deths and, consequently, larger regenerator and heat exchanger gas. This allows for easier heat exchanger fabrication, which is adantageous for closed thermoacoustic engine alications [16]. Howeer, the closed configuration is restrictie in the outut of acoustic waes in oen saces. Therefore, some researchers hae gien their attention to deeloing other alications. In 1, Slaton [17] constructed an oen-air standingwae thermoacoustic system. The maximum acoustic ressure radiated from the oen end of their resonator corresonded to 81 db Sound Pressure Leel (SPL) ref μpa (1 μpa 1 6 Pa) for an inut electric ower of 76 W. He concluded that a higher ower ersion of that deice may be used as a continuous source at low frequency. The standing-wae thermoacoustic system is a simle configuration and allows for easy oscillation, because of the relatiely low required onset temerature. Howeer, theoretically, the thermal efficiency of this system is lower than that of a traeling-wae thermoacoustic system because the standing-wae system has an irreersible thermal cycle [16]. Therefore, the erformance of this oen standing-wae system is limited. Comared with an oen standing-wae system, an oen traeling-wae thermoacoustic system has a higher onset temerature and is more difficult to design. Howeer, this system can be used to design as acoustic generator with higher ower outut, because of its Stirling thermal cycle. This can significantly increase the maximum acoustic ressure comared with Slaton s system. Inestigations into oen-air thermoacoustic systems are in their initial hases. In addition, a comarable closed system has not been reorted in the literature. Therefore, we roose an oen-air traeling-wae thermoacoustic generator. In this aer, taking the inut and reflected waes into account, a theoretical model on the acoustic imedance at the end and at the inut of the system were deried by soling the acoustic roagation equation. Comarisons of a closed acoustic configuration with an oen system while accounting for the influence of ressure, olumetric elocity, imedance and acoustic work were analyzed in detail. n oen-air traeling-wae thermoacoustic generator was designed and fabricated. Exerimental measurements of the ressure waeforms, and acoustic ressures at the oen end and at.1 m,.3 m and.5 m from the oen end at different heating owers were erformed. The acoustic ressures with and without a cone were comared. The maximum acoustic ressure at the oen end of the resonator was db (ref μpa) for a heating ower of 1 W. 1 Oen-air traeling-wae thermoacoustic generator The acoustic configuration of the traditional traeling-wae thermoacoustic engine is comosed of a looed tube and a closed resonator. Thermoacoustic comonents such as regenerators and heat exchangers are inserted into the looed tube as shown in Figure 1(a). We adoted an oen resonator in our traeling-wae thermoacoustic generator. The acoustic wae roagates in the oen-air sace, which is shown in Figure 1(b). The essential difference between the closed and oen acoustic configurations is the end of resonator. closed thermoacoustic system has a stable boundary condition. Different mean ressures and gas tyes can be used and can be adjusted for erformance otimization according to the needs of the intended alication. n oen thermoacoustic system is oen to the atmoshere, meaning the oerating arameters are limited because the system must oerate at 1 bar in air. Therefore, in this aer, the differences between the closed and oen acoustic configurations are emhasized. Theoretical comarisons of closed and an oen acoustic configuration The thermoacoustics that occur in the regenerator of looed tube can be simlified and treated as an acoustic source to analyze the influence of the closed or an oen acoustic configuration in the system. These configurations are shown are in Figure 1(a) and (b). The continuity of the ressure and the elocity are assured at the surface of the looed tube that is connected to the resonator. This surface, namely the inut of the resonator, is set to be the origin of the x-coordinate. Here, the acoustic imedance is Z a. The length of resonator is l, and the acoustic imedance at the end of resonator is Z al. This simle acoustic configuration is shown in Figure. Figure 1 Schematic diagram of thermoacoustic system. (a) Closed traeling-wae thermoacoustic engine; (b) oen-air traeling-wae thermoacoustic generator.

3 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. 169 Figure Simle model of acoustic configuration of the thermoacoustic system. The work roduced by the thermoacoustic effect in regenerator in the looed tube is transferred to the resonator. The ressure, 1, can be decomosed into the inut wae i and the reflected wae r, because of the endca of the resonator. i and r are exressed as i ai e i(ωt+kx) and r ai e i(ωt kx), resectiely. Here ar e i σ r r π, r is the ai reflected coefficient, σ π is the hase difference at the interface of the inut and reflected waes. Therefore, 1 is defined as ( + σπ) iωt ( ω + φ) ikx ikx i t 1 i + r ai e + r e e 1 e, (1) where ressure amlitude is 1 λ ai 1+ r + r cosk x+ σ 4, and φ is the constant hase. ccording to the definition of the elocity, 1 can be searated to i and r, where and r is gien by i t kx ar i t kx are e ρa i ( ω ) ( ω ) i t kx ai i t kx aie e ρa ( ω + ) ( ω + ). Therefore the elocity 1 + i r 1 i r. ρa ρa () Combining eqs. (1) and (), the secific acoustic imedance along the resonator is found to be ikx ikx 1 aie + are Zs ρa. (3) ikx ikx 1 aie are We can eliminate ai and ar by utting the secific acoustic imedances at x and xl into eq. (3). lso, the secific acoustic imedance at x can be exressed as one at x1. From this we find Z Zsl + iρa tan kl ρ a. ρ a + iz tan kl s sl Therefore, the acoustic imedance at x can be exressed as one at x1: ρa ρ al a Z + i tan kl Za, (5) ρa + izal tan kl where is the cross-sectional area, ρ and a are the density (4) and acoustic seed of the gas, resectiely. ( γ ) f ( ε ) ω 1+ 1 k / 1+ k a 1 f s is comlex wae number. ω and γ are the angular frequency and ratio of isobaric and ( 1+ i) δk isochoric secific heats, resectiely. Here, fk r ( 1+ i) δ and f. r is the radius of the resonator. The r k κ thermal enetration deth, δ k, ωρ c ω and the iscous enetration deth, μ ν δ ωρ ω, indicate how far heat and momentum can diffuse laterally during a time interal on the order of the eriod of the oscillation 1/ kρc diided by π. ε s, and k, κ, μ, ν and c are the ksρscs thermal conductiity, thermal diffusiity, dynamic diffusiity, kinematic iscosity, and isobaric heat caacity er unit mass of gas, resectiely. k s, ρ s and c s are the thermal conductiity, density and heat caacity er unit mass of solid, resectiely. (1) When the end has a closed endca, xl, Z al, eq. (5) simlifies to ρa Za i cot( kl). (6) Eq. (6) shows that the characteristics at the inut the resonator are related to the alue kl. The length of resonator is usually chosen to be in the range l(1/4 1/)λ in the thermoacoustic system. Then, kl l π 1+ ( γ 1 ) fk /( 1+ ε s) λ 1 f ( γ ) f ( ε ) 1+ 1 k / 1+ s ( π/ π), 1 f where λ is the waelength. The acoustic imedance is a function of the dimensions of the resonator, the mean ressure, the resonant frequency and the roerties of the gas. () When the end is oen to air, for the condition of low frequency kr<1, the acoustic imedance at the end of the resonator is similar to the acoustic radiation of a limitless baffle late. That is, Z al R al +ix al, where the real art 4 ρak πr is Ral, and the imaginary art is X al

4 17 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. 8 3 akr. 3 ρ Eq. (5) can now be simlified to Z a ρ a ρa Ral + i Xal + tan kl. ρa X al tan kl + iral tan kl (7) Eqs. (6) and (7) show that the acoustic imedance at the inut of the resonator is correlated with the dimensions of the resonator, the mean ressure, the resonant frequency and the roerties of the gas. Therefore, for gien resonator dimensions and a fixed resonant frequency, the differences between a closed and an oen acoustic configuration can be quantitatiely analyzed based on the linear thermoacoustic model [16]. For a closed acoustic configuration, the resonator has two arts, one is L1 with a length of.53 m and the other is L with a length of 1 m, in which are filled with 1 bar and 5 bar of air, resectiely. For an oen acoustic configuration, a tube with a diameter of.5 m and a length of 1 m relaces L. It has the same olume and length as a room. Then the end of L1 can be aroximated as being oen to the atmoshere. The oerating arameters and roerties of the gas are listed in Table 1 for the closed and oen acoustic configurations. The frequency was maintained at 74 Hz, and the ariational range is about 3 Hz in the simulation. Therefore, the influence of frequency on the system can be ignored. From this, both the closed and oen acoustic configurations were ealuated. The influence of the ressure, olumetric elocity, imedance and acoustic work were considered and are lotted in Figures 3(a), 3(b), 4 and 5. The influences of the closed and oen acoustic configurations on the ressure amlitude, 1, and the olumetric elocity amlitude, U 1, along the length of the system are shown in Figure 3. When the end is closed, the minimum ressure amlitude occurs at x.53 m, not at the end of the resonator. The waeform of 1 is about 3/4 waelength. The ariational trend of U 1 is the oosite of 1 and has it maximum at x.53 m. lso, it reaches zero at the end of resonator. The closed system can be filled with high ressure gas. 1 is significantly enhanced at a mean ressure of 5 bar in air. Howeer, U 1 decreases, which shows that the imedance increases and iscous losses decrease with U 1. When the end is oen, the minimum alue of 1 is equal to zero and is at x.53 m. The waeform of 1 is 1/4 waelength. U 1 in the oen system is similar to that in the closed system. Comared with the closed acoustic configuration, the oen configuration at same mean ressure can achiee a higher 1 and U 1. Howeer, 1 is significantly lower and U 1 much greatly higher when the oen configuration is comared to the closed with 5 bar air. Note that the acoustic ressure at the end of the resonator should be high for alications, but it is at its minimum alue. This contradiction comes into being from two different mechanisms, and it is the key to allow the oen system to significantly imroe the acoustic ressure at the end of resonator. Figure 4 shows the imedance amlitude, Z 1, along the length in the closed and oen acoustic configurations. For the closed acoustic configuration, Z 1 reaches a maximum between at the end of resonator. This is caused by the antinode of 1 and node of U 1. Z 1 initially decreases and then increases, after reaching a minimum at x.53 m. For the oen acoustic configuration, Z 1 has the maximum of 1 6 at the inut and the decreases to zero at the oen end. Table 1 Oerating arameters and gas roerties (ambient temerature 3 K) coustic configuration Gas tye Mean ressure (bar) Frequency (Hz) Thermal enetration deth (μm) Viscous enetration deth (μm) air Closed end air Oen end air Figure 3 Pressure amlitude and olumetric elocity amlitude along the length in the closed and oen acoustic configuration. (a) Pressure amlitude; (b) olumetric elocity amlitude.

5 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. 171 Z 1 along the interal between.53 m is nearly equal for both closed and oen systems at a mean ressure of 1 bar air. It is helful to fill the resonator with to a high ressure to imroe Z 1. The acoustic work, Ė, done in the closed and oen acoustic configurations is shown in Figure 5. It was inferred 1 1 u1 ma from the relationshi: E ~ 1 U1 ~, and m a that a higher Ė can be acquired for higher alues of 1 and U 1. The total Ė roduced in the oen system is 5.6 W, and.38 W is transferred into the oen resonator. Howeer, Ė dissiates raidly to zero at the oen end. For the closed acoustic configuration, the total Ė is W, and.94 W is transferred at 5 bar. t 1 bar, the total is.85 W, and the amount transferred is 1.4 W. In both of the closed configurations the Ė transorted into resonator dissiates gradually to zero at the closed end. We concluded from the aboe inestigations that the oen system has a higher 1, U 1 and Ė relatie to the closed system at the same ressure. 1 and Ė are lower in the 1 bar oen system comared with those in the 5 bar closed system. It is difficult to design an oen system, because of the raid losses in 1 and Ė at the oen end. Fortunately, acoustic radiation can be used for long-range roagation, which was not included in this model. Therefore, it is otimal for a 1/4 waelength system to use acoustic amlified comonents to imroe the erformance of the system. Based on linear thermoacoustic equations [16] and the aboe analysis, an oen-air traeling-wae thermoacoustic generator was designed and fabricated. 3 Exerimental setu Figure 4 Imedance amlitude along the length in the closed and oen acoustic configurations. Figure 5 coustic work along the length in the closed and oen acoustic configurations. The exerimental setu of the oen-air traeling-wae thermoacoustic generator is shown in Figure 6 and is comosed of three arts: a looed tube, a resonator and a cone. The looed tube is comosed of a comliance tube, inertance tube and some thermoacoustic comonents. These include a hot and cold heat exchangers and a regenerator. Eight iezoelectric ressure sensors for measuring the ressure amlitude are laced along the system, and are indicated as P 1 P 8 in Figure 6. In the looed tube, the ressure dro in heat exchanger, comared with that in the regenerator, was small and negligible. Therefore the ressure, which was measured using sensor P 1 as a reference, was distributed at the inut of cold heat exchanger. Sensor P was laced at the outut of the comliance tube to measure the ressure dro. Pressure sensors P 3 P 8 were used to measure ressure losses in the inertance tube, through regenerator, thermal buffer tube and resonator, resectiely. In addition, measured ressures could be analyzed using the acoustic field distribution and ressure waeform. Sensor P 9 was an acoustimeter with high sensitiity, which was used to acquire the acoustic ressure far away from the outut of the resonator. Thermocoules T 1 T 3 were laced in the middle of heater and at the two ends of regenerator. They were used to simultaneously measure the temerature at the two ends of regenerator and the onset temerature of system. T 1 and T were Ni Cr thermocoules, and T 3 was a Cu Cu thermocoule. The looed tube assured that the hase difference in ressure that generates the olumetric elocity near the regenerator is matched to the traeling-wae hase. The gas arcel initiates the Stirling thermal cycle within the enetration deth of the regenerator. The resonator stabilizes the resonant frequency, increases the acoustic imedance near the regenerator, and transfers the acoustic ower. The cone imroes the SPL at the outut of system. This generator is smaller than 1 m in length and.3 m in height. 4 Results and discussion The ressure amlitudes 1, which were measured using P 1 P 8, are shown in Figure 7. During these measurements, the heating ower was 1 W. In Figure 7, it can be seen that 1 was at its maximum near the cold heat exchanger. long counterclockwise direction in the looed tube, 1 steadily decreased from P to P 5, and in the resonator from P 6 to P 8. The eak-to-eak ressure amlitude (P-P ressure

6 17 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. Figure 6 Exerimental setu of the oen-air traeling-wae thermoacoustic generator. amlitude) at P 1 was 4.6 kpa and the SPL was db. e This was calculated by using SPL log1 db, where e was the measured ressure and equal to P-P ressure amlitude here, ref was the referenced ressure with the alue of 1 5 Pa in the air. The uer surface of cold heat exchanger was set at the origin of x-coordinate. Unfolding the looed tube in counterclockwise direction along the comliance tube, the inertance tube was at a negatie osition in x, and in the clockwise direction, the cold heat exchanger, regenerator, thermal buffer tube and resonator were at ositie ositions in x. The ressure amlitude along the length of the system was analyzed and shown in Figure 8 for arious heating owers. The P-P ressure amlitude increased as the heating ower increased. The resonant frequency was 74 Hz, and the acoustic seed was 347 m/s when the ambient air temerature was 3 K. Therefore the waelength of system was λa/f, Figure 7 Pressure amlitudes ersus time measured by ressure sensors P 1 P 8. ref Figure 8 Peak-to-eak ressure amlitude along the length of the system measured by ressure sensors P 1 P 8. which was 4.75 m. The waeform of the P-P ressure amlitude was nearly 1/4 waelength. The effect of the cone on the acoustic ressure exressed as SPL radiated from the oen end of the resonator was inestigated for arious heating owers Q h. The results are shown in Figure 9. Without the cone, the SPL attenuated linearly with distance toward the oen end of the resonator. The attenuation of the SPL could be reduced effectiely using the cone for identical heating owers. In Figure 9, the results are shown with and without the cone at a heating ower of 145 W. The SPL.5 m far away from the oen end of resonator was about 95 db, and increased nearly 15 db when the cone was added. The maximum acoustic ressure at the oen end and.5 m away from the oen end of the resonator were db and 11 db (ref μpa) for a heating ower of 1 W, resectiely. The arameters, including onset temerature T onset, the temerature in the heater T heater, the hot temerature T h, the cold temerature T c and the acoustic ressure at the oen end of resonator, are

7 Xie X J, et al. Chinese Sci Bull July (11) Vol.56 No. 173 listed in Table for heating owers of 145 W and 1 W with and without the cone. Using the cone significantly decreased the onset temerature and the temerature in the heater. The absolute temerature ratio between the two ends of regenerator is defined as τt h /T c. The acoustic ower has a direct ratio with τ. lower temerature in the heater means that more heating ower can be added to the system, which is imortant for achieing a large τ. Therefore, more acoustic ower and a higher SPL can be acquired with the cone. With further inestigations into the configuration and the line tye of the cone, the SPL at the oen end of the resonator could be otimized. 5 Conclusions In this aer, we designed and fabricated an oen-air traeling-wae thermoacoustic generator. This design has the adantages of being small and haing a simle configuration. We comared the closed and oen acoustic configurations in detail. We modeled the effects on the ressure, olumetric elocity, imedance and acoustic work. We concluded that the oen system has a higher 1, U 1 and Ė relatie to the closed system for the same mean ressure (1 bar air). 1 and Ė are lower in the 1 bar oen system than in the 5 bar closed system. In the oen system the modeled waeform had a 1 of a 1/4 waelength system in which 1 and Ė dissiated raidly at the oen end. Based on the aboe analysis, we fabricated a 1 bar oen-air thermoacoustic Figure 9 coustic ressure ersus the distance to the oen end of the resonator. Table Cone Oerating arameters, temerature and acoustic ressure Heating ower Temerature ( C) (W) Onset T 1 T T 3 coustic ressure (db) Without With generator. It had a maximum acoustic ressure of db near sensor P 1 at the cold heat exchanger. The cone at the oen end of the resonator reduces the onset temerature and the temerature in the heater. This increased the absolute temerature ratio and acoustic ressure. The maximum acoustic ressures at the oen end and.5 m from the oen end of the resonator were db and 11 db (ref μpa) for a heating ower of 1 W, resectiely. This is suitable for ractical use as a low-frequency acoustic source. In future work, we hoe to achiee an SPL of 15 db. t this leel, the deice could be a ossible solution for some of the roblems of existing acoustic generators, which include low acoustic ressures and system comlexity. We beliee this system can be used as a basic acoustic source for low frequency and long-range noise exeriments, and as a suly for high acoustic ressures for studying industrial sources and ibrations. This work was suorted by the National Natural Science Foundation of China (58681). 1 Swift G W. Thermoacoustic engines. J coust Soc m, 1988, 84: Feldman K T. Reiew of the literature on Sondhauss thermoacoustic henomena. J Sound Vib, 1968, 7: Wheatley J C, Hofler T, Swift G W, et al. n intrinsically irreersible thermoacoustic heat engine. J coust Soc m, 1983, 74: Ceerley P H. istonless Stirling engine-the traeling wae heat engine. J coust Soc m, 1979, 66: Yazaki T, Maekawa T, Tominaga, et al. Traeling wae thermoacoustic engine in a looed tube. Phys Re Lett, 1998, 81: Backhaus S, Swift G W. thermoacoustic Stirling heat engine. Nature, 1999, 399: Gardner D L, Swift G W. cascade thermoacoustic engine. J coust Soc m, 3, 114: Hu Z J, Li Q, Li Q, et a1. high frequency cascade thermoacoustic engine. Cryogenics, 6, 46: Radebaugh R. reiew of ulse tube refrigeration. d Cryo Eng B, 199, 35: Jin T, Chen G B, Shen Y. thermoacoustically drien ulse tube refrigerator caable of working below 1K. Cryogenics, 1, 41: Sun D M, Marc D, Guenter T, et al. Inestigation on regenerator temerature inhomogeneity in Stirling-tye ulse tube cooler. Chinese Sci Bull, 9, 54: Zhou G, Li Q, Li Z Y, et al. Influence of resonator diameter on a miniature thermoacoustic Stirling heat engine. Chinese Sci Bull, 8, 53: Hu J Y, Luo E C, Li S F, et al. Heat-drien thermoacoustic cryocooler oerating at liquid hydrogen temerature with a unique couler. J l Phys, 8, 13: Backhaus S, Tward E, Petach M. Traeling-wae thermoacoustic electric generator. l Phys Lett, 4, 85: Luo E C, Wu Z H, Dai W, et al. 1W-class traeling-wae thermoacoustic electricity generator. Chinese Sci Bull, 8, 53: Swift G W. Thermoacoustics: Unifying Persectie for Some Engines and Refrigerators. Sewickley, P: coustical Society of merica Publishers, 17 Slaton W V. n oen-air infrasonic thermoacoustic engine. l coust, 1, 71: 36 4 Oen ccess This article is distributed under the terms of the Creatie Commons ttribution License which ermits any use, distribution, and reroduction in any medium, roided the original author(s) and source are credited.

Production and Detection Theory of Pulsed Photoacoustic Wave with Maximum Amplitude and Minimum Distortion in Absorbing Liquid

Production and Detection Theory of Pulsed Photoacoustic Wave with Maximum Amplitude and Minimum Distortion in Absorbing Liquid roduction and Detection Theory of ulsed hotoacoustic Wae with Maximum mlitude and Minimum Distortion in bsorbing iquid Zuomin Zhao, Seo Nissilä, Onni hola, Risto Myllylä bstract The hotoacoustic effect

More information

AE301 Aerodynamics I UNIT A: Fundamental Concepts

AE301 Aerodynamics I UNIT A: Fundamental Concepts AE301 Aerodynamics I UNIT A: Fundamental Concets ROAD MAP... A-1: Engineering Fundamentals Reiew A-: Standard Atmoshere A-3: Goerning Equations of Aerodynamics A-4: Airseed Measurements A-5: Aerodynamic

More information

JJMIE Jordan Journal of Mechanical and Industrial Engineering

JJMIE Jordan Journal of Mechanical and Industrial Engineering JJMIE Jordan Journal of Mechanical and Industrial Engineering Volume, Number, Jun. 8 ISSN 995-6665 Pages 7-75 Efficiency of Atkinson Engine at Maximum Power Density using emerature Deendent Secific Heats

More information

COMPUTER SIMULATION OF A LABORATORY HYDRAULIC SYSTEM WITH MATLAB-SIMULINK

COMPUTER SIMULATION OF A LABORATORY HYDRAULIC SYSTEM WITH MATLAB-SIMULINK DVNCED ENGINEERING 4(20101, ISSN 1846-5900 COMPUTER SIMULTION OF LORTORY HYDRULIC SYSTEM WITH MTL-SIMULINK Grego, G. & Siminiati, D. bstract: The article resents some selected roblems related to modeling

More information

Design of Standing Wave Type Thermoacoustic Prime Mover for 300 Hz Operating Frequency

Design of Standing Wave Type Thermoacoustic Prime Mover for 300 Hz Operating Frequency Design of Standing Wave Type Thermoacoustic Prime Mover for 300 Hz Operating Frequency S.M.Mehta 1, K.P.Desai 2, H.B.Naik 2, M.D.Atrey 3 1 L. D. College of Engineering, Ahmedabad, Gujarat, India 2 S. V.

More information

Entransy analysis of open thermodynamic systems

Entransy analysis of open thermodynamic systems Article Engineering hermohysics August 0 Vol.57 No.: 934940 doi: 0.007/s434-0-54-x Entransy analysis of oen thermodynamic systems CHENG Xueao, WANG WenHua & LIANG XinGang * Key Laboratory for hermal Science

More information

Distribution of populations in excited states of electrodeless discharge lamp of Rb atoms

Distribution of populations in excited states of electrodeless discharge lamp of Rb atoms Article Atomic & Molecular Physics June 2013 Vol.58 No.16: 18761881 doi: 10.1007/s11434-013-5789-z Distribution of oulations in excited states of electrodeless discharge lam of Rb atoms TAO ZhiMing 1,2,

More information

Biomechanical Analysis of Contemporary Throwing Technique Theory

Biomechanical Analysis of Contemporary Throwing Technique Theory MAEC Web of Conferences, 0 5 04 ( 05 DOI: 0.05/ matec conf / 0 5 0 5 04 C Owned by the authors, ublished by EDP Sciences, 05 Biomechanical Analysis of Contemorary hrowing echnique heory Jian Chen Deartment

More information

Homogeneous and Inhomogeneous Model for Flow and Heat Transfer in Porous Materials as High Temperature Solar Air Receivers

Homogeneous and Inhomogeneous Model for Flow and Heat Transfer in Porous Materials as High Temperature Solar Air Receivers Excert from the roceedings of the COMSOL Conference 1 aris Homogeneous and Inhomogeneous Model for Flow and Heat ransfer in orous Materials as High emerature Solar Air Receivers Olena Smirnova 1 *, homas

More information

Chapter 9 Practical cycles

Chapter 9 Practical cycles Prof.. undararajan Chater 9 Practical cycles 9. Introduction In Chaters 7 and 8, it was shown that a reversible engine based on the Carnot cycle (two reversible isothermal heat transfers and two reversible

More information

C H A P T E R ,1752'8&7,21

C H A P T E R ,1752'8&7,21 CHAPTER The first law of thermodynamics is a secial case of the fundamental and general law of conseration of energy, which is alied to thermal henomena in thermodynamic system. The basic law of energy

More information

The extreme case of the anisothermal calorimeter when there is no heat exchange is the adiabatic calorimeter.

The extreme case of the anisothermal calorimeter when there is no heat exchange is the adiabatic calorimeter. .4. Determination of the enthaly of solution of anhydrous and hydrous sodium acetate by anisothermal calorimeter, and the enthaly of melting of ice by isothermal heat flow calorimeter Theoretical background

More information

Chapter 1 Fundamentals

Chapter 1 Fundamentals Chater Fundamentals. Overview of Thermodynamics Industrial Revolution brought in large scale automation of many tedious tasks which were earlier being erformed through manual or animal labour. Inventors

More information

300 kpa 77 C. (d) If we neglect kinetic energy in the calculation of energy transport by mass

300 kpa 77 C. (d) If we neglect kinetic energy in the calculation of energy transport by mass 6-6- Air flows steadily a ie at a secified state. The diameter of the ie, the rate of flow energy, and the rate of energy transort by mass are to be determed. Also, the error oled the determation of energy

More information

A Critical State Sand Model with Elastic-Plastic Coupling

A Critical State Sand Model with Elastic-Plastic Coupling A Critical State Sand Model with Elastic-Plastic Couling Ali Lashkari * and Ali Golchin Deartment of Ciil & Enironmental Engineering Shiraz Uniersity of Technology, Shiraz, Iran lashkari@sutech.ac.ir,

More information

INVESTIGATION OF AERATED SIPHON

INVESTIGATION OF AERATED SIPHON INVETIGATION OF AERATED IPHON Detlef Aigner, Hans-B. Horlacher Institute for Hydraulic Engineering and Alied Hydromechanics, Dresden Uniersity of Technology, 006 Dresden, Germany, hone: +49 35 46334397;

More information

Speed of sound measurements in liquid Methane at cryogenic temperature and for pressure up to 10 MPa

Speed of sound measurements in liquid Methane at cryogenic temperature and for pressure up to 10 MPa LNGII - raining Day Delft, August 07 Seed of sound measurements in liquid Methane at cryogenic temerature and for ressure u to 0 MPa Simona Lago*, P. Alberto Giuliano Albo INRiM Istituto Nazionale di Ricerca

More information

Computational Acoustic Attenuation Performance of Helicoidal Resonators Comparable to Experiment

Computational Acoustic Attenuation Performance of Helicoidal Resonators Comparable to Experiment Comutational Acoustic Attenuation Perormance o Helicoidal Resonators Comarable to Exeriment PhD. Eng. Wojciech LAPKA Poznan University o Technology Institute o Alied Mechanics Division o Vibroacoustics

More information

Fast Modeling of Phase Changes in a Particle Injected Within a d.c Plasma Jet

Fast Modeling of Phase Changes in a Particle Injected Within a d.c Plasma Jet Thermal Sray 2007: Global Coating Solutions (Ed.) B.R. Marle, M.M. Hyland, Y.-C. Lau, C.-J. Li, R.S. Lima, and G. Montaon Published by ASM International, Materials Park, Ohio, USA, Coyright 2007 Fast Modeling

More information

COMPENDIUM OF EQUATIONS Unified Engineering Thermodynamics

COMPENDIUM OF EQUATIONS Unified Engineering Thermodynamics COMPENDIUM OF EQUAIONS Unified Engineering hermodynamics Note: It is with some reseration that I suly this comendium of equations. One of the common itfalls for engineering students is that they sole roblems

More information

On the relationship between sound intensity and wave impedance

On the relationship between sound intensity and wave impedance Buenos Aires 5 to 9 Setember, 16 Acoustics for the 1 st Century PROCEEDINGS of the nd International Congress on Acoustics Sound Intensity and Inverse Methods in Acoustics: Paer ICA16-198 On the relationshi

More information

Roots Blower with Gradually Expanding Outlet Gap: Mathematical Modelling and Performance Simulation Yingjie Cai 1, a, Ligang Yao 2, b

Roots Blower with Gradually Expanding Outlet Gap: Mathematical Modelling and Performance Simulation Yingjie Cai 1, a, Ligang Yao 2, b 2nd International Conference on Advances in Mechanical Engineering and Industrial Informatics (AMEII 216) Roots Bloer ith Gradually Exanding Outlet Ga: Mathematical Modelling and Performance Simulation

More information

Study of the circulation theory of the cooling system in vertical evaporative cooling generator

Study of the circulation theory of the cooling system in vertical evaporative cooling generator 358 Science in China: Series E Technological Sciences 006 Vol.49 No.3 358 364 DOI: 10.1007/s11431-006-0358-1 Study of the circulation theory of the cooling system in vertical evaorative cooling generator

More information

Nonlinear superheat and capacity control of a refrigeration plant

Nonlinear superheat and capacity control of a refrigeration plant Nonlinear suerheat and caacity control of a refrigeration lant Henrik Rasmussen Deartment of Electronic Systems Aalborg University DK-92 Aalborg, Denmark Email: hr@es.aau.dk Lars F. S. Larsen Danfoss A/S,

More information

Node-voltage method using virtual current sources technique for special cases

Node-voltage method using virtual current sources technique for special cases Node-oltage method using irtual current sources technique for secial cases George E. Chatzarakis and Marina D. Tortoreli Electrical and Electronics Engineering Deartments, School of Pedagogical and Technological

More information

02. Equilibrium Thermodynamics II: Engines

02. Equilibrium Thermodynamics II: Engines University of Rhode Island DigitalCommons@URI Equilibrium Statistical Physics Physics Course Materials 205 02. Equilibrium Thermodynamics II: Engines Gerhard Müller University of Rhode Island, gmuller@uri.edu

More information

T. Yazaki Department of Physics, Aichi University, Kariya 448, Japan

T. Yazaki Department of Physics, Aichi University, Kariya 448, Japan Experimental studies of a thermoacoustic Stirling prime mover and its application to a cooler Y. Ueda, a) T. Biwa, and U. Mizutani Department of Crystalline Materials Science, Nagoya University, Nagoya

More information

The Numerical Simulation of Gas Turbine Inlet-Volute Flow Field

The Numerical Simulation of Gas Turbine Inlet-Volute Flow Field World Journal of Mechanics, 013, 3, 30-35 doi:10.436/wjm.013.3403 Published Online July 013 (htt://www.scir.org/journal/wjm) The Numerical Simulation of Gas Turbine Inlet-Volute Flow Field Tao Jiang 1,

More information

The directivity of the forced radiation of sound from panels and openings including the shadow zone

The directivity of the forced radiation of sound from panels and openings including the shadow zone The directivity of the forced radiation of sound from anels and oenings including the shadow zone J. Davy RMIT University, Alied Physics, GPO Box 476V, 3001 Melbourne, Victoria, Australia john.davy@rmit.edu.au

More information

The time and space characteristics of magnetomotive force in the cascaded linear induction motor

The time and space characteristics of magnetomotive force in the cascaded linear induction motor J. Mod. Transort. (13) 1(3):194 199 DOI 1.17/s434-13-18-7 The time and sace characteristics of magnetomotive force in the cascaded linear induction motor Dajing Zhou Jiaqing Ma Lifeng Zhao Xiao Wan Yong

More information

ADVANCEMENT OF SMALL-SCALE THERMOACOUSTIC ENGINE

ADVANCEMENT OF SMALL-SCALE THERMOACOUSTIC ENGINE ADVANCEMENT OF SMALL-SCALE THERMOACOUSTIC ENGINE By SUNGMIN JUNG Masters in Mechanical Engineering WASHINGTON STATE UNIVERSITY School of Mechanical and Material Engineering MAY 2009 To the Faculty of Washington

More information

E o e associated with a light field (both the real part and the. ikr t. under the assumptions that J free

E o e associated with a light field (both the real part and the. ikr t. under the assumptions that J free Reiew Problems Chaters 1-5 True and False Questions E1. T or F: The otical index of any material aries with frequency. E2. T or F: The frequency of light can change as it enters a crystal. E3. T or F:

More information

A. G. Falkowski Chrysler Corporation, Detroit, Michigan 48227

A. G. Falkowski Chrysler Corporation, Detroit, Michigan 48227 Three-ass mufflers with uniform erforations A. Selamet V. Easwaran The Ohio State University, Deartment of Mechanical Engineering Center for Automotive Research, 06 West 18th Avenue, Columbus, Ohio 4310

More information

Numerical thermo-hydro-mechanical modeling of compacted bentonite in China-mock-up test for deep geological disposal

Numerical thermo-hydro-mechanical modeling of compacted bentonite in China-mock-up test for deep geological disposal Journal of Rock Mechanics and Geotechnical Engineering. 212, 4 (2): 183 192 Numerical thermo-hydro-mechanical modeling of comacted bentonite in China-mock-u test for dee geological disosal Liang Chen 1,

More information

Lecture 8, the outline

Lecture 8, the outline Lecture, the outline loose end: Debye theory of solids more remarks on the first order hase transition. Bose Einstein condensation as a first order hase transition 4He as Bose Einstein liquid Lecturer:

More information

A Four-Quadrant Thrust Estimation Scheme Based on Chebyshev Fit and Experiment of Ship Model

A Four-Quadrant Thrust Estimation Scheme Based on Chebyshev Fit and Experiment of Ship Model Send Orders of Rerints at bssaif@emirates.net.ae 148 The Oen Mechanical Engineering Journal, 2012, 6, (Sul 2: M5) 148-154 Oen Access A Four-uadrant Thrust Estimation Scheme Based on Chebyshe Fit and Exeriment

More information

Application of Automated Ball Indentation for Property Measurement of Degraded Zr2.5Nb

Application of Automated Ball Indentation for Property Measurement of Degraded Zr2.5Nb Journal of Minerals & Materials Characterization & Engineering, Vol. 10, No.7,.661-669, 011 jmmce.org Printed in the USA. All rights reserved Alication of Automated Ball Indentation for Proerty Measurement

More information

16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE

16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE 16. CHARACTERISTICS OF SHOCK-WAVE UNDER LORENTZ FORCE AND ENERGY EXCHANGE H. Yamasaki, M. Abe and Y. Okuno Graduate School at Nagatsuta, Tokyo Institute of Technology 459, Nagatsuta, Midori-ku, Yokohama,

More information

Class 17: The Uncertainty Principle

Class 17: The Uncertainty Principle Class 7: The Uncertainty Princile Wae ackets and uncertainty A natural question to ask is if articles behae like waes, what is waing? The arying quantity is related to the robability of finding the article

More information

MODELING AND SIMULATION OF REFORMER AUTO- THERMAL REACTOR IN AMMONIA UNIT

MODELING AND SIMULATION OF REFORMER AUTO- THERMAL REACTOR IN AMMONIA UNIT Peet trool lleeuum & Cooaal ll IISSN 337-77 Available online at www.vuru.sk/c Petroleum & Coal 9 (), 6-7, 7 MODELING AND SIMULATION OF REFORMER AUTO- THERMAL REACTOR IN AMMONIA UNIT Kayvan Khorsand *,

More information

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS HET, ORK, ND THE FIRST L OF THERMODYNMIS 8 EXERISES Section 8. The First Law of Thermodynamics 5. INTERPRET e identify the system as the water in the insulated container. The roblem involves calculating

More information

FINITE TIME THERMODYNAMIC MODELING AND ANALYSIS FOR AN IRREVERSIBLE ATKINSON CYCLE. By Yanlin GE, Lingen CHEN, and Fengrui SUN

FINITE TIME THERMODYNAMIC MODELING AND ANALYSIS FOR AN IRREVERSIBLE ATKINSON CYCLE. By Yanlin GE, Lingen CHEN, and Fengrui SUN FINIE IME HERMODYNAMIC MODELING AND ANALYSIS FOR AN IRREVERSIBLE AKINSON CYCLE By Yanlin GE, Lingen CHEN, and Fengrui SUN Performance of an air-standard Atkinson cycle is analyzed by using finite-time

More information

On Gravity Waves on the Surface of Tangential Discontinuity

On Gravity Waves on the Surface of Tangential Discontinuity Alied Physics Research; Vol. 6, No. ; 4 ISSN 96-9639 E-ISSN 96-9647 Published by anadian enter of Science and Education On Gravity Waves on the Surface of Tangential Discontinuity V. G. Kirtskhalia I.

More information

On Line Parameter Estimation of Electric Systems using the Bacterial Foraging Algorithm

On Line Parameter Estimation of Electric Systems using the Bacterial Foraging Algorithm On Line Parameter Estimation of Electric Systems using the Bacterial Foraging Algorithm Gabriel Noriega, José Restreo, Víctor Guzmán, Maribel Giménez and José Aller Universidad Simón Bolívar Valle de Sartenejas,

More information

Feedback-error control

Feedback-error control Chater 4 Feedback-error control 4.1 Introduction This chater exlains the feedback-error (FBE) control scheme originally described by Kawato [, 87, 8]. FBE is a widely used neural network based controller

More information

Study on Characteristics of Sound Absorption of Underwater Visco-elastic Coated Compound Structures

Study on Characteristics of Sound Absorption of Underwater Visco-elastic Coated Compound Structures Vol. 3, No. Modern Alied Science Study on Characteristics of Sound Absortion of Underwater Visco-elastic Coated Comound Structures Zhihong Liu & Meiing Sheng College of Marine Northwestern Polytechnical

More information

Improved Perfectly Matched Layers for Acoustic Radiation and Scattering Problems

Improved Perfectly Matched Layers for Acoustic Radiation and Scattering Problems NATO Undersea Research Centre Partnering for Maritime Innovation Presented at the COMSOL Conference 008 Hannover Acoustics Session Wed 5 November 008, 13:00 15:40. Imroved Perfectly Matched Layers for

More information

ANALYTICAL MODEL FOR THE BYPASS VALVE IN A LOOP HEAT PIPE

ANALYTICAL MODEL FOR THE BYPASS VALVE IN A LOOP HEAT PIPE ANALYTICAL MODEL FOR THE BYPASS ALE IN A LOOP HEAT PIPE Michel Seetjens & Camilo Rindt Laboratory for Energy Technology Mechanical Engineering Deartment Eindhoven University of Technology The Netherlands

More information

Journal of System Design and Dynamics

Journal of System Design and Dynamics Vol. 5, No. 6, Effects of Stable Nonlinear Normal Modes on Self-Synchronized Phenomena* Hiroki MORI**, Takuo NAGAMINE**, Yukihiro AKAMATSU** and Yuichi SATO** ** Deartment of Mechanical Engineering, Saitama

More information

Synthetic Jet Cooling Part I: Overview of Heat Transfer and Acoustics

Synthetic Jet Cooling Part I: Overview of Heat Transfer and Acoustics Synthetic Jet Cooling Part I: Oeriew of Heat Transfer and Acoustics Clemens J.M. Lasance 1, Ronald M. Aarts 1,2 1 Philis Research Laboratories, 2 Eindhoen Uniersity of Technology High Tech Camus 4, 5656

More information

MODELING AND SIMULATION OF A SATELLITE PROPULSION SUBSYSTEM BY PHYSICAL AND SIGNAL FLOWS. Leonardo Leite Oliva. Marcelo Lopes de Oliveira e Souza

MODELING AND SIMULATION OF A SATELLITE PROPULSION SUBSYSTEM BY PHYSICAL AND SIGNAL FLOWS. Leonardo Leite Oliva. Marcelo Lopes de Oliveira e Souza Satellite Proulsion Subsystem MODELING AND SIMULATION OF A SATELLITE PROPULSION SUBSYSTEM BY PHYSICAL AND SIGNAL FLOWS Leonardo Leite Oliva National Institute for Sace Research, INPE Av. dos Astronautas,

More information

Approach to canonical pressure profiles in stellarators

Approach to canonical pressure profiles in stellarators 1 TH/P8-4 Aroach to canonical ressure rofiles in stellarators Yu.N. Dnestroskij 1), A.. Melniko 1), L.G. Elisee 1), S.E. Lysenko 1), K.A. Razumoa 1),.D. Pustoito 1), A. Fujisawa ), T. Minami ), and J.H.

More information

Lecture 13. Heat Engines. Thermodynamic processes and entropy Thermodynamic cycles Extracting work from heat

Lecture 13. Heat Engines. Thermodynamic processes and entropy Thermodynamic cycles Extracting work from heat Lecture 3 Heat Engines hermodynamic rocesses and entroy hermodynamic cycles Extracting work from heat - How do we define engine efficiency? - Carnot cycle: the best ossible efficiency Reading for this

More information

Passive Mechanical Device for Phase Shifting in a Pulse Tube Cryocooler

Passive Mechanical Device for Phase Shifting in a Pulse Tube Cryocooler C19_018 1 Passive Mechanical Device for Phase Shifting in a Pulse Tube Cryocooler D. Radchenko 1, G. Grossman Ricor Cryogenic and Vacuum Systems, Ein Harod Ihud, Israel Technion Israel Institute of Technology,

More information

THE FIRST LAW OF THERMODYNAMICS

THE FIRST LAW OF THERMODYNAMICS THE FIRST LA OF THERMODYNAMIS 9 9 (a) IDENTIFY and SET UP: The ressure is constant and the volume increases (b) = d Figure 9 Since is constant, = d = ( ) The -diagram is sketched in Figure 9 The roblem

More information

Aalborg Universitet. Nonlinear superheat and capacity control of a refrigeration plant Rasmussen, Henrik; Larsen, Lars F. S.

Aalborg Universitet. Nonlinear superheat and capacity control of a refrigeration plant Rasmussen, Henrik; Larsen, Lars F. S. Aalborg Universitet Nonlinear suerheat and caacity control of a refrigeration lant Rasmussen, Henrik; Larsen, Lars F. S. Published in: 17th Mediterranean Conference on Control and Automation DOI (link

More information

Chapter 6: Sound Wave Equation

Chapter 6: Sound Wave Equation Lecture notes on OPAC0- ntroduction to Acoustics Dr. Eser OLĞAR, 08 Chater 6: Sound Wave Equation. Sound Waves in a medium the wave equation Just like the eriodic motion of the simle harmonic oscillator,

More information

Notes on pressure coordinates Robert Lindsay Korty October 1, 2002

Notes on pressure coordinates Robert Lindsay Korty October 1, 2002 Notes on ressure coordinates Robert Lindsay Korty October 1, 2002 Obviously, it makes no difference whether the quasi-geostrohic equations are hrased in height coordinates (where x, y,, t are the indeendent

More information

Experimental Investigation on a Single-Stage Stirling-Type Pulse Tube Cryocooler Working below 30 K

Experimental Investigation on a Single-Stage Stirling-Type Pulse Tube Cryocooler Working below 30 K Experimental Investigation on a Single-Stage Stirling-Type Pulse Tube Cryocooler Working below 30 K J. Ren 1, 2, W. Dai 1, E. Luo 1, X. Wang 1, 2, J. Hu 1 1 Chinese Academy of Sciences, Beijing 100190,

More information

arxiv: v1 [math-ph] 21 Dec 2007

arxiv: v1 [math-ph] 21 Dec 2007 Dynamic Phase ransitions in PV Systems ian Ma Deartment of Mathematics, Sichuan Uniersity, Chengdu, P. R. China Shouhong Wang Deartment of Mathematics, Indiana Uniersity, Bloomington, IN 4745 (Dated: February

More information

Prediction of the Excitation Force Based on the Dynamic Analysis for Flexible Model of a Powertrain

Prediction of the Excitation Force Based on the Dynamic Analysis for Flexible Model of a Powertrain Prediction of the Excitation Force Based on the Dynamic Analysis for Flexible Model of a Powertrain Y.S. Kim, S.J. Kim, M.G. Song and S.K. ee Inha University, Mechanical Engineering, 53 Yonghyun Dong,

More information

PHYSICAL REVIEW LETTERS

PHYSICAL REVIEW LETTERS PHYSICAL REVIEW LETTERS VOLUME 81 20 JULY 1998 NUMBER 3 Searated-Path Ramsey Atom Interferometer P. D. Featonby, G. S. Summy, C. L. Webb, R. M. Godun, M. K. Oberthaler, A. C. Wilson, C. J. Foot, and K.

More information

ONE. The Earth-atmosphere system CHAPTER

ONE. The Earth-atmosphere system CHAPTER CHAPTER ONE The Earth-atmoshere system 1.1 INTRODUCTION The Earth s atmoshere is the gaseous enveloe surrounding the lanet. Like other lanetary atmosheres, it figures centrally in transfers of energy between

More information

Integrated optics acousto-optic polarization analyzer sensor

Integrated optics acousto-optic polarization analyzer sensor Integrated otics acousto-otic olarization analyzer sensor Luiz Poffo a, Pierre Lemaître-Auger b, Philie Benech c, Pierre Benech c a A PHOTONIC SENSORS, 3 Parvis Louis Néel - BP 57-38016 Grenoble cedex

More information

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics PHYS1001 PHYSICS 1 REGULAR Module Thermal Physics Chater 17 First Law of Thermodynamics References: 17.1 to 17.9 Examles: 17.1 to 17.7 Checklist Thermodynamic system collection of objects and fields. If

More information

Actual exergy intake to perform the same task

Actual exergy intake to perform the same task CHAPER : PRINCIPLES OF ENERGY CONSERVAION INRODUCION Energy conservation rinciles are based on thermodynamics If we look into the simle and most direct statement of the first law of thermodynamics, we

More information

Estimation of dynamic behavior and energy efficiency of thrust hybrid bearings with active control

Estimation of dynamic behavior and energy efficiency of thrust hybrid bearings with active control INTERNATIONAL JOURNAL OF MECHANICS Volume 1 18 Estimation of dynamic behavior and energy efficiency of thrust hybrid bearings with active control Alexander Babin Sergey Majorov Leonid Savin Abstract The

More information

Lecture 13 Heat Engines

Lecture 13 Heat Engines Lecture 3 Heat Engines hermodynamic rocesses and entroy hermodynamic cycles Extracting work from heat - How do we define engine efficiency? - Carnot cycle: the best ossible efficiency Reading for this

More information

Engineering Thermodynamics. Chapter 4. The First Law of Thermodynamics

Engineering Thermodynamics. Chapter 4. The First Law of Thermodynamics Chater 4 The First Law of Thermodynamics It is the law that relates the arious forms of energies for system of different tyes. It is simly the exression of the conseration of energy rcile The first law

More information

Study on a Ship with 6 Degrees of Freedom Inertial Measurement System and Related Technologies

Study on a Ship with 6 Degrees of Freedom Inertial Measurement System and Related Technologies Oen Access Library Journal Study on a Shi with 6 Degrees of Freedom Inertial Measurement System and Related echnologies Jianhui Lu,, Yachao Li, Shaonan Chen, Yunxia Wu Shandong rovince Key Laboratory of

More information

Experimental acoustic identification of flow noise sources in expansion chambers

Experimental acoustic identification of flow noise sources in expansion chambers Exerimental acoustic identification of flow noise sources in exansion chambers W. De Roeck, W. Desmet K.U.Leuven, Deartment of Mechanical Engineering, Celestijnenlaan 300 B, B-3001, Leuven, Belgium e-mail:

More information

Finite-Sample Bias Propagation in the Yule-Walker Method of Autoregressive Estimation

Finite-Sample Bias Propagation in the Yule-Walker Method of Autoregressive Estimation Proceedings of the 7th World Congress The International Federation of Automatic Control Seoul, Korea, July 6-, 008 Finite-Samle Bias Proagation in the Yule-Walker Method of Autoregressie Estimation Piet

More information

Piston Surface Pressure of Piston- Cylinder System with Finite Piston Speed

Piston Surface Pressure of Piston- Cylinder System with Finite Piston Speed 44, Issue (08) 55-5 Journal of Adanced Research in Fluid Mechanics and Thermal Sciences Journal homeage: www.akademiabaru.com/arfmts.html ISSN: 89-7879 Piston Surface Pressure of Piston- Cylinder System

More information

Wolfgang POESSNECKER and Ulrich GROSS*

Wolfgang POESSNECKER and Ulrich GROSS* Proceedings of the Asian Thermohysical Proerties onference -4 August, 007, Fukuoka, Jaan Paer No. 0 A QUASI-STEADY YLINDER METHOD FOR THE SIMULTANEOUS DETERMINATION OF HEAT APAITY, THERMAL ONDUTIVITY AND

More information

Flexible Pipes in Trenches with Stiff Clay Walls

Flexible Pipes in Trenches with Stiff Clay Walls Flexible Pies in Trenches with Stiff Clay Walls D. A. Cameron University of South Australia, South Australia, Australia J. P. Carter University of Sydney, New South Wales, Australia Keywords: flexible

More information

High speed wind tunnels 2.0 Definition of high speed. 2.1 Types of high speed wind tunnels

High speed wind tunnels 2.0 Definition of high speed. 2.1 Types of high speed wind tunnels Module Lectures 6 to 1 High Seed Wind Tunnels Keywords: Blow down wind tunnels, Indraft wind tunnels, suersonic wind tunnels, c-d nozzles, second throat diffuser, shocks, condensation in wind tunnels,

More information

Available online at ScienceDirect. Procedia Engineering 102 (2015 )

Available online at  ScienceDirect. Procedia Engineering 102 (2015 ) Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 1 (15 ) 3 38 The 7th World Congress on Particle Technology (WCPT7) Characterization of Colloidal Particles using Electrical

More information

Introduction to Thermodynamic Cycles Part 1 1 st Law of Thermodynamics and Gas Power Cycles

Introduction to Thermodynamic Cycles Part 1 1 st Law of Thermodynamics and Gas Power Cycles Introduction to Thermodynamic Cycles Part 1 1 st Law of Thermodynamics and Gas Power Cycles by James Doane, PhD, PE Contents 1.0 Course Oeriew... 4.0 Basic Concepts of Thermodynamics... 4.1 Temperature

More information

OPTIMAL DESIGN AND OPERATION OF HELIUM REFRIGERATION SYSTEMS USING THE GANNI CYCLE

OPTIMAL DESIGN AND OPERATION OF HELIUM REFRIGERATION SYSTEMS USING THE GANNI CYCLE OPTIMAL DESIGN AND OPERATION OF HELIUM REFRIGERATION SYSTEMS USING THE GANNI CYCLE V. Ganni, P. Knudsen Thomas Jefferson National Accelerator Facility (TJNAF) 12000 Jefferson Ave. Newort News, VA 23606

More information

KEY ISSUES IN THE ANALYSIS OF PILES IN LIQUEFYING SOILS

KEY ISSUES IN THE ANALYSIS OF PILES IN LIQUEFYING SOILS 4 th International Conference on Earthquake Geotechnical Engineering June 2-28, 27 KEY ISSUES IN THE ANALYSIS OF PILES IN LIQUEFYING SOILS Misko CUBRINOVSKI 1, Hayden BOWEN 1 ABSTRACT Two methods for analysis

More information

5 Diagnosis of diesel engines

5 Diagnosis of diesel engines 5 Diagnosis of diesel engines In order to develo advanced fault-detection and diagnosis systems for diesel engines a modular structure is used, which is based on the available inut and outut signals from

More information

Factors Effect on the Saturation Parameter S and there Influences on the Gain Behavior of Ytterbium Doped Fiber Amplifier

Factors Effect on the Saturation Parameter S and there Influences on the Gain Behavior of Ytterbium Doped Fiber Amplifier Australian Journal of Basic and Alied Sciences, 5(12): 2010-2020, 2011 ISSN 1991-8178 Factors Effect on the Saturation Parameter S and there Influences on the Gain Behavior of Ytterbium Doed Fiber Amlifier

More information

A Comprehensive Study on a Latent Heat Thermal Energy Storage System and its Feasible Applications in Greenhouses

A Comprehensive Study on a Latent Heat Thermal Energy Storage System and its Feasible Applications in Greenhouses Iranian Journal of Chemical Engineering Vol. 13, No. 2 (Sring 2016, IAChE A Comrehensive Study on a Latent Heat Thermal Energy Storage System and its Feasible Alications in reenhouses A. Mirahmad 1, S.

More information

Numerical Simulation of Particle Concentration in a Gas Cyclone Separator *

Numerical Simulation of Particle Concentration in a Gas Cyclone Separator * 2007 Petroleum Science Vol.4 No.3 Numerical Simulation of Particle Concentration in a Gas Cyclone Searator * Xue Xiaohu, Sun Guogang **, Wan Gujun and Shi Mingxian (School of Chemical Science and Engineering,

More information

Numerical Simulation and Experimental of Residual Stress Field of SAE1070 Spring Steel Induced by Laster Shock

Numerical Simulation and Experimental of Residual Stress Field of SAE1070 Spring Steel Induced by Laster Shock Research Journal of Alied Sciences, Engineering and Technology 5(20): 4869-4877, 203 ISSN: 2040-7459; e-issn: 2040-7467 Maxwell Scientific Organization, 203 Submitted: Setember 27, 202 Acceted: November,

More information

Thermoacoustic analysis of a pulse tube refrigerator

Thermoacoustic analysis of a pulse tube refrigerator Journal of Physics: Conference Series Thermoacoustic analysis of a pulse tube refrigerator To cite this article: T Biwa 2012 J. Phys.: Conf. Ser. 400 052001 View the article online for updates and enhancements.

More information

TEVATRON LUMINOSITY UPGRADE PROJECT *

TEVATRON LUMINOSITY UPGRADE PROJECT * TEVATRON LUMINOSITY UPGRADE PROJECT John P. Marriner, Fermilab, Batavia, IL, USA Abstract Fermilab has embarked on a luminosity ugrade for the Tevatron. The major comonents of this ugrade are the Main

More information

University of North Carolina-Charlotte Department of Electrical and Computer Engineering ECGR 4143/5195 Electrical Machinery Fall 2009

University of North Carolina-Charlotte Department of Electrical and Computer Engineering ECGR 4143/5195 Electrical Machinery Fall 2009 University of North Carolina-Charlotte Deartment of Electrical and Comuter Engineering ECG 4143/5195 Electrical Machinery Fall 9 Problem Set 5 Part Due: Friday October 3 Problem 3: Modeling the exerimental

More information

Oil Temperature Control System PID Controller Algorithm Analysis Research on Sliding Gear Reducer

Oil Temperature Control System PID Controller Algorithm Analysis Research on Sliding Gear Reducer Key Engineering Materials Online: 2014-08-11 SSN: 1662-9795, Vol. 621, 357-364 doi:10.4028/www.scientific.net/kem.621.357 2014 rans ech Publications, Switzerland Oil emerature Control System PD Controller

More information

Modelling a Partly Filled Road Tanker during an Emergency Braking

Modelling a Partly Filled Road Tanker during an Emergency Braking Proceedings of the World Congress on Engineering and Comuter Science 217 Vol II, October 25-27, 217, San Francisco, USA Modelling a Partly Filled Road Tanker during an Emergency Braking Frank Otremba,

More information

INTRODUCING THE SHEAR-CAP MATERIAL CRITERION TO AN ICE RUBBLE LOAD MODEL

INTRODUCING THE SHEAR-CAP MATERIAL CRITERION TO AN ICE RUBBLE LOAD MODEL Symosium on Ice (26) INTRODUCING THE SHEAR-CAP MATERIAL CRITERION TO AN ICE RUBBLE LOAD MODEL Mohamed O. ElSeify and Thomas G. Brown University of Calgary, Calgary, Canada ABSTRACT Current ice rubble load

More information

Meshless Methods for Scientific Computing Final Project

Meshless Methods for Scientific Computing Final Project Meshless Methods for Scientific Comuting Final Project D0051008 洪啟耀 Introduction Floating island becomes an imortant study in recent years, because the lands we can use are limit, so eole start thinking

More information

Ultrasound Beam Focusing Considering the Cutaneous Fat Layer Effects

Ultrasound Beam Focusing Considering the Cutaneous Fat Layer Effects Ultrasound Beam Focusing Considering the Cutaneous Fat Layer Effects A. B. M. Aowlad Hossain 1*, Laehoon H. Kang 1 Deartment of Electronics and Communication Engineering Khulna University of Engineering

More information

Theoretical Analysis on Deflagration-to-Detonation Transition *

Theoretical Analysis on Deflagration-to-Detonation Transition * heoretical Analysis on Deflagration-to-Detonation ransition * Yun-Feng Liu( 刘云峰 ),**, Huan Shen( 沈欢 ),, De-Liang Zhang( 张德良 ),, Zong-Lin Jiang( 姜宗林 ), Institute of echanics, Chinese Academy of Sciences,

More information

9.3 Laminar Flat-Plate Boundary Layer: Exact Solution w-19

9.3 Laminar Flat-Plate Boundary Layer: Exact Solution w-19 9.3 Laminar Flat-Plate Boundary Layer: Exact Solution w-19 Laminar Flat-Plate Boundary Layer: Exact Solution The solution for the laminar boundary layer on a horizontal flat late was obtained by Prtl s

More information

Phase transition. Asaf Pe er Background

Phase transition. Asaf Pe er Background Phase transition Asaf Pe er 1 November 18, 2013 1. Background A hase is a region of sace, throughout which all hysical roerties (density, magnetization, etc.) of a material (or thermodynamic system) are

More information

Analysis of Pressure Transient Response for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia

Analysis of Pressure Transient Response for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia roceedings World Geothermal Congress 00 Bali, Indonesia, 5-9 Aril 00 Analysis of ressure Transient Resonse for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia Jorge A.

More information

Physics 2A (Fall 2012) Chapters 11:Using Energy and 12: Thermal Properties of Matter

Physics 2A (Fall 2012) Chapters 11:Using Energy and 12: Thermal Properties of Matter Physics 2A (Fall 2012) Chaters 11:Using Energy and 12: Thermal Proerties of Matter "Kee in mind that neither success nor failure is ever final." Roger Ward Babson Our greatest glory is not in never failing,

More information

Chapter 12: Three-Phase Circuits

Chapter 12: Three-Phase Circuits Chater 1: Three-Phase Circuits 1.1 ntroduction 1. Balanced Three-Phase oltages 1.3 Balanced Wye-Wye connection 1.4 Balanced Wye-Delta Connection 1.7 Power in a Balanced System 1.1 NTRODUCTON A single-hase

More information

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential Chem 467 Sulement to Lectures 33 Phase Equilibrium Chemical Potential Revisited We introduced the chemical otential as the conjugate variable to amount. Briefly reviewing, the total Gibbs energy of a system

More information