Investigation of passive acoustic anemometer by use of wind noise correlation

Size: px
Start display at page:

Download "Investigation of passive acoustic anemometer by use of wind noise correlation"

Transcription

1 Investigation of passive acoustic anemometer by use of wind noise correlation Tetsuro MURAKAMI 1, Yoshinori YOKO, Yuya SATO 3, Hirofumi NAKAJIMA 4, Kazuhiro NAKADAI Kogakuin University, Japan 5 Honda Research Institute Japan, Japan ABSTRACT This paper examines feasibility of an acoustic anemometer by evaluating estimates of wind directions and wind velocities towards microphone array. These estimates are calculated based on a number of delay times among pair-microphones. To obtain the delay times, a low-frequency correlation of coherence function between wind noises for pair-microphones is practically utilized. This paper firstly discusses about the validity of the estimation method for wind direction and wind velocity by means of simulated wind noises to obtain some high-precision results. Secondly, the estimation accuracies of the wind directions and the wind velocities are evaluated for wind noises recorded in a practical environment. The winds are generated by a tower fan and recorded by three microphones that are closely located at each vertex of a triangle. The results for the recorded wind noises show that estimation errors are heavily dependent on the recording direction in contrast to the results for the simulated wind noises. Since these fluctuations of the errors are commonly observed in several recorded wind noises, a correction for unknown estimates is approximately calculated by employing some known estimates and their errors. As a result, the average relative error of the wind velocity was 5.4 % and the average absolute error of the wind direction was 6.64 deg. This correction method indicated the efficacy of estimating the wind directions and the wind velocities. Keywords: Anemometer, Wind noise, Correlation function I-INCE Classification of Subjects Number(s):.3 1. INTRODUCTION Wind direction (WD) and wind velocity (WV) used for the weather forecast or the damage prediction due to a typhoon are measured in a few ways, for example, a cup anemometer or a vane anemometer using the dynamics of wind itself, a hot-wire anemometer using the cooling effect of air passing on a wire, a sonic anemometer using delay time of ultrasonic sound waves between pairs of transducers (1). In the field of acoustic signal processing, there are studies about the estimation of WD and WV using wind noise. The wind noises are observed when wind blows to a diaphragm of microphones. In the estimation of WV by means of a single microphone, there are some previous studies that spectrum distribution of wind noises dependent on WV () or higher order correlations of wind noises (3) are utilized. In addition, there are studies that WV including WD is estimated using multi microphones (4,5). An anemometer based on wind noises is not active anemometer such as sonic anemometer and does not move dynamically such as cup anemometer, therefore wind noise has an advantage of estimation WV and WD. However, there are no discussions in the previous studies about any implementation of anemometer for practical use. 1 t.murakami@cc.kogakuin.ac.jp j1317@ns.kogakuin.ac.jp 3 j11346@ns.kogakuin.ac.jp 4 nakajima@cc.kogakuin.ac.jp 5 nakadai@jp.honda-ri.com 67

2 Figure 1 The relationship between wind and a pair-microphone.. PURPOSE AND APPROACH This paper aims at constructing a system of a passive acoustic anemometer by means of multi microphones. It has been found a low-frequency correlation between wind noises for closely allocated pairmicrophones, and a peak of the correlation function corresponds to not the speed of sound but the wind speed(6). Therefore, the multi microphones are closely allocated each other, and WD and WV are estimated from the delay time between microphone outputs. Section 3 explains an estimation method for WD and WV, and then Section 4 tries to test the efficacy of the estimation method by simulated wind noises. In Section 5, WD and WV are estimated based on wind noises recorded by a microphone array system. In Section 6, the estimation error occurred in Section 5 is reduced by a correction using the relationship between estimates and references. 3. ESTIMATION OF WD, WV First, the delay times, which are the differences of arrival time between microphone pairs, are estimated by the correlation of recorded wind noises. Next, a wind vector composed of WD as the direction and WV as the norm is calculated using the estimated delay times. 3.1 Estimation of wind vector Figure 1 shows the relationship between a column wind vector v and the delay time at the microphones M 1 and M. Defining the location of M 1 as a reference position, the location of M is expressed by a column vector, x 1. Here, the wind around the micprophone is expressed as the column wind vector v, which is -dimentional vector and lies in the same plane as x 1. The relationship between the delay time t and the position vector x 1 is given as t = x 1 v cos θ 1 = x 1 v = x T v v 1 v, (1) where θ 1 is the angle between x 1 and v and v is L norm of v. In Equation (1), even if x 1 and t are known, -dimentional v is non-unique. Therefore, the wind vector is estimated using three microphones M 1, M and M 3. Generalizing x 1 to x ij, assume that x ij is a position column vector indicating the position of M j referred to the position of M 1 and t ij is the delay time corresponding to x ij. Given the delay times vector t =(t 1 t 3 t 13 ) T and the microphones position matrix X =(x 1 x 3 x 13 ) T, Equation (1) is extended as t = X v v. () Now presuming that X is known, it can be considered that the wind vector ˆv is estimated using the delay time ˆt, which is also estimated from the wind noises. Using each error of the estimated delay times e = ˆt t, the relationship among the wind vector, the delay time and the microphone-array in Equation () is modeled as ˆt = X ˆv + e. (3) ˆv 68

3 Estimating the wind vector ˆv using the criterion of the least mean-square error, the following equation is obtained as ˆv ˆv = X+ˆt, (4) where X + is the pseudo inverse matrix of X. Taking square of L norm for both sides of the Equation (4), the equation is 1 ˆv = X+ˆt. (5) Substitute Equation (5) in Equation (4), the estimated wind vector is obtained as, The estimated wind direction ˆθ is calculated as ˆv = X+ˆt. (6) X +ˆt ˆθ =tan 1 ˆv, (7) where tan 1 is the fourth-quadrant inverse tangent function, and the range of the WD is 18 ˆθ < Estimation of delay times This section explains the estimation method of the delay times for wind noises which are utilized for the estimation of the wind vector. Wind noise recorded by the microphone pair has a correlation in coherence function (6). The delay time in sample ˆτ is calculated based on a peak of the cross-correlation function for a pair of wind noises. Defined that n is the index of discrete time, the recorded wind noises m i (n) and m j (n) are obtained from the microphones M i and M j respectively. After m i (n) and m j (n) are divided into K frames with frame length L and shift length S, each of k-th frame is expressed as m i (n, k) and m j (n, k) respectively. The estimated delay time ˆτ ij (k) in sample is expressed as ˆτ ij (k) = arg max γ(n, k), (8) n where the absolute value of the delay time τ ij (k) is assumed to be smaller than L/, and the range of L/ < ˆτ ij (k) <L/ regarding m i (n, k),m j (n, k) as a periodic signal. Note that the cross-correlation function in this paper is calculated using fast Fourier transform F and its inverse transform F 1 as, γ(n, k) =F 1 {F{m i (n, k)} F{m j (n, k)}}, (9) where {} denotes the complex conjugate of {}. The estimated delay time ˆt ij is obtained using the average of the estimate delay in sample ˆτ ij = ˆτ ij (k) as, where f s is the sampling frequency of the recorded wind noises. ˆt ij = ˆτ ij f s, (1) 4. VALIDATION OF THE ESTIMATION METHOD BY COMPUTER SIMULATION To validate the estimation method for wind vector, wind noises recorded by the microphone array are generated by a computer simulation and the wind vectors are estimated based on the wind noise signals. 69

4 Figure Allocation of the microphone array Table 1 Estimation error for WD (deg) and WV (m/s) in the simulation WD WV Maximum of error Minimum of error Average of error Standard deviation of error Wind noises generated by a computer simulation First the microphone position matrix X is prepared by allocating microphones on microphone array, then WD and WV composing the wind vector are defined as a reference. Next, the delay time vector t is given by substituting X and v into Equation (). A wind noise recorded by the method shown in section 5 is allocated in channel 1 as a reference. The signal in channel i is the signal shifting channel 1 by the delay time in sample τ 1i corresponding to t 1i. If zero intervals in either channel are occurred due to the shifting process, the intervals of all channels are eliminated. In the simulation, 3 microphones M 1, M and M 3 in the microphone array are allocated at each vertex of a 4mm equilateral triangle shown in Figure. The direction from the center of the triangle to the microphone M 1 is defined as deg. for WD. The angle increases in a counterclockwise direction, and if the angle reaches up to 18 deg., then it becomes -18 deg. For this simulation, 1 wind vectors were generated, whose WDs were from -18 deg. to 177 deg. having an interval of 3 deg. and WVs were 3.5 m/s equally. In the case of calculating the delay time, the frame length was L = 15 = 3768 samples, the shift length was S = 11 = 48 samples and the FFT length was equal to the frame length. 4. Result of the simulation Table 1 shows the estimation error of WD and WV in the simulation. Each error in the table is shown in the absolute value. As the average error of WD was 1.5 deg. and the average relative error of WV was.6%, the estimation method was successful to indicate the efficacy in principle. Their errors are probably due to rounding from delay time t 13 to delay sample τ 1 when channels are shifting. 5. EVALUATION OF THE ESTIMATION ACCURACY IN ACTUAL ENVIRONMENT This section explains evaluation of the estimated wind vector. Wind noises are recorded by the actual microphone array. 5.1 Recording Method 3 microphones in the microphone array had the same allocation depicted in Figure 3. The microphones were omnidirectional AV-LEADER s TCM37 and the wind screen was disused in order to record the wind noises. As a wind generator, YUASA s tower fan YT-776NR was used, and the distance to microphones was adjusted so that recorded WVs were from 1. m/s to 3.5 m/s at an interval of.5 m/s, in total 6 steps of WVs. To measure a reference for WV, the averaged WV for 4 seconds was obtained by CELESTRON s Wind Guide 7

5 Figure 3 Microphone array Figure 4 Anemometer for measuring a reference of WV Figure 5 A photo of recording environment Figure 6 Angles according to the frame length L, l, the shift length S, s. 381 shown in Figure 4. WD was controlled using the microphone array placed on GSI Creos s rotating table DS1 which rotates.3 deg/s in clockwise direction. For each recording of WV, the wind noises were recorded for 1 rotation (36 deg.). Apart from the simulation, since WD changes continuously, the wind vector was estimated frame by frame basis with the frame length l and the shift length s. To obtain a reference for WD, a proportional relationship between the rotation time and the rotation angle was used. 5. Recording Environment Figure 5 shows the recording environment for wind noises. A program called pa-wavplay of MATLAB (3bit) was employed for the multi-channel recording. The output signals from the microphone array were amplified by AUDIO TECHNICA S AT-MA and saved on the computer via Roland s audio devices OCTA- CAPTURE. The sampling frequency for the recording was 44.1 khz. 5.3 Frame processing of recorded wind noises To analyze the recorded wind noises, dual frame processing was performed. Figure 6 shows the frame processing with the angles according to the frame length and the shift length. Note that the angles are depicted about 1 times larger than the actual size for clarity. Using previous frame processing for wind vector, the continuous angles in each frame were regarded as stationary signal. Processing for the wind vector divides signals into frames whose length l = 17 = 1317 samples and shift length s = 14 = samples using Hanning window. Next frame processing for delay time has a role of averaging the continuous change for the delay time in each wind noise divided by previous frame processing. In frame processing for delay time, the frame length is L = 15 = 3768 samples and the shift length is S = 11 = 48 samples, and Hanning window is used. 5.4 Results of the estimation and discussion This subsection shows the results of the estimation and discusses about the results. 71

6 Estimated direction (deg) Estimated velocity (m/s) Estimated value True value True direction (deg) Estimted value True value True direction (deg) 6 3 (m/s) Locus of true vectors Estimated vectors -6-1 velocity Figure 7 Estimated WD (upper figure) and WV (lower figure). Solid line and chained line indicate the estimated values and the reference values respectively. Figure 8 The overview of the wind vectors in each recorded frame. Each wind vector indicates the arrival direction, and its magnitude expresses WV. A chained circle is a locus of the reference for wind vectors Effects on the estimated wind vectors by the recorded WD Figure 7 shows the estimated WV and WD which varies dependent on the recorded WD. Figure 8 shows the overview of the estimated wind vectors in each recorded frame. From these figures, it is found that the errors of the estimated WD and WV depended on the actual WD. The estimated WD and WV have a rotational symmetry at every 1 deg.: WDs have an oscillation about deg. for every 1 deg. and WVs have 3 intervals of being convex upward in every 1 deg. This symmetry seems to be caused by the triangular allocation of microphones on the microphone array. Especially, at WDs about deg., 1 deg., -1 deg., where the WD was from the front of the microphones, the slope observed in the estimated WD was the largest and the estimated WV was very close to the reference at the center of the intervals being convex upward observed in the estimated WV. On the other hand, at WDs about 6 deg., -6 deg. and -18 deg., where the WD was from between the microphones, the slope for the oscillation observed in the estimated WD was the smallest and the error of the estimated WV became larger. It is considered that the change of the estimated wind vectors in the recorded WDs was due to turbulence caused by the wind blowing to the side surface of microphones and the wind reduced WV around microphones. Figure 9 illustrates variation of WV in cases of that the recorded WDs were, 1 or -1 deg., 6, -6 or -18 deg. and others. In case of, 1 or -1 deg. (Figure 9a), as the wind blowing to the front of microphone flows along with rim of microphone, the turbulence is not occured. In case of 6, -6, or -18 deg. (Figure 9b), as the wind blowing from between microphones hits the microphone array, the turbulence is occurred. As the turbulence interfered the wind over the microphone array and reduced its WV, and also the longer delay times of the wind noises were estimated, slower WVs were obtained. In other cases, such that the allocation of the microphone array is asymmetry for the wind blowing to the microphone array (Figure 9c), a part of the wind over the microphone is strongly affected by the turbulence but some parts of the wind are unaffected. Consequently, since WVs were different each other between microphones and the delay times were larger than it should be, the false estimation was occurred such that WD changed. The cause of this false estimation could be based on the understanding such as WV is invariant around the microphone array. 7

7 (a) deg, 1 deg -1 deg (b) 6 deg, -6 deg -18 deg (c) Other cases Figure 9 The variation of WV by the recorded WD. The white arrows illustrate winds over the microphone array, the black arrows express winds at the same height as microphones. 18 Estimated direction (deg) m/s 3.5m/s True direction (deg) Estimated velocity (m/s) Average of maximum Average of all frames Average of minimum True velocity (m/s) Figure 1 The relationship between estimated WD and recorded WD. Light and dark solid lines express the estimates of recorded WVs, 1. and 3.5 m/s respectively. Figure 11 The relationship between the estimated WV and the recorded WV 5.4. Effects on the estimated wind vectors by the recorded WV Figure 1 shows the relationship between the estimated WD and the reference. The fluctuation of the estimated WVs for both 1. and 3.5 m/s were equally affected by the recorded WD, and the other recorded WVs between 1.5 and 3. m/s were also affected. On the other hand, the variance of the error for each WD was larger and the estimation accuracy was lower as WV was slower. Figure 11 shows the relationship between the estimated WV and the reference for the wind noises having WVs from 1. to 3.5 m/s. The estimated WVs for each wind noise vary widely depending on the recorded WDs as well as the estimated WDs. 3 Polygonal lines composed of the average estimated WV over all frames, the mean value of 3 maximum values for each interval of every 1 deg., and the mean value of 3 minimum values for each interval of every 1 deg., were drawn. From the figure, the mean value of 3 maximum values was larger than the reference by.1-.3 m/s in case of that the recorded WV was faster than. m/s. Therefore, the tendency that the estimated WV gets closer to the reference at deg., 1 deg. and -1 deg. can be observed at the different recorded WV. However, in case of that the recorded WV was slower than. m/s, the mean value of 3 maximum values tended to be 1 m/s larger than the reference. In addition, the slope of each line is smaller than that of the recorded WV was faster than. m/s. As shown in the above results of the estimated WD and WV, the estimated wind vectors is more accurate as the recorded WV is faster. Since the frequency bands that the wind noise is observed increases as WV is faster (), the information to calculate the correlation also increases. This leads better estimation accuracy of 73

8 the delay time. 6. CORRECTION OF ESTIMATE WIND VECTOR There was a fluctuation of the error in the estimated wind vector according to the recorded WD. This error of the estimated wind vector is corrected based on the fluctuation. 6.1 Correction method In section 5, the wind vector was estimated by the microphone array. At the same time, the reference of the wind vector was measured by the anemometer and the rotating table having an constant angular velocity. The estimated wind vector (referred to as "the estimated vector" lator on) and the reference are defined as u and u true respectively. The correction vector c(u) for u is defined as c(u) =u true u. (11) However, the reference is unavailable when the wind vector is estimated using only microphone array. Defining the estimated vector as w whose reference is unavailable, the correction vector c(w) is also unavailable. To avoid this, a dataset consisted of u and u true is prepared in advance, and then the estimated vector is corrected by calculating an approximation of the correction vector ĉ(w). The approximation of the correction vector ĉ(w) is obtained as ĉ(w) = 1 R(w) u R(w) where R(w) is defined as a set of u within a radius r from w, such as c(u), (1) R(w) ={u U; r u w }. (13) 6. Correction for the estimated vector and the evaluation New wind noises whose WV is.5 m/s are recorded as the estimated vectors w, but the reference w true is also measured in order to investigate the error after the correction. The wind noise recorded in Section 5 is utilized as the estimated vector u whose reference is available. To indicate how much the error is reduced before and after the correction, Error reduction ratio is defined as (Error reduction ratio) = 1 (Error after correction) (Error before correction). (14) Figure 1 shows the Error reduction ratio in WD and WV according to the radius r. The Error reduction ratio reached a maximum 39 % in WV at r =.18 and76%inwdatr =.13. Figure 13 shows the estimated WV and WD after the correction at r =.18. Table shows the estimation error before and after the correction. The correction was effective for WV whose error was large before the correction, and the averaged error for WV after the correction was.135 m/s. On the other hand, the correction was ineffective for WD whose error was small before the correction, and the averaged error for WD after the correction was 6.64 deg. By applying the correction to the estimated vector, the error of WD was reduced from 1.8 deg. to 6.64 deg. and the relative error of WV was reduced from 1.9 % to 5.4 % for the reference of.5 m/s. Consequently, WD and WV were well estimated towards the reference, and the efficacy of the correction was observed. 7. CONCLUSION WD and WV were estimated by means of small size microphone array and the acoustical anemometer was designed. As the fluctuation of WD and WV due to the form of microphone was observed, it was corrected to reduce the errors of the estimates. For high-precise estimation, the design of microphone array and the 74

9 Error reduction ratio Velocity Direction r Figure 1 The relationship between Error reduction ratio and radius r. Solid line and chained line express WV and WD respectively. Estimated velocity (m/s) Estimated direction (deg) 3.5 Estimated value 1.5 True value Corrected value True direction (deg) Estimted value True value Corrected value True direction (deg) Figure 13 The estimated WV (upper figure) and WD (lower figure) after correction. Solid line and chained line express the estimated values and the reference values respectively. Table Estimation error for WD (deg) and WV (m/s) before and after correction Before After WD WV WD WV Maximum of error Minimum of error Average of error Standard deviation of error improvement of the correction method should be reconsidered as future works so that the whole system could have less errors. Moreover, for the implementation of a practical anemometer, concerning the real time processing and expanding the microphone array system to 3-dimentional would be important tasks. REFERENCES 1. Ito M. The Story of the Wind I ( I). GIHODO SHUPPAN; Japan p Sugano K, Chiba N. Development of a Microphone-based Wind Velocity Sensor and Its Application to Real-time Animation of a Tree Swaying in Real World Wind. The Journal of the Society for Art and Science; Japan 7. p Fujita Y, Ota M, Takakuwa Y. A Principle for Measurement Method of Wind Speed Using Higher Order Correlation Information between Wind Noise and Wind Speed. Acoust. Soc. Jap Spring Meeting, Japan 1998(1). p Bass, Henry E. and Raspet, Richard and Messer, John O. Experimental determination of wind speed and direction using a three microphone array. J. Acoust. Soc. Am., 97; p Godin, Oleg A. and Irisov, Vladimir G. and Charnotskii, Mikhail I. Passive acoustic measurements of wind velocity and sound speed in air. J. Acoust. Soc. Am., 135; 14. p

10 6. Sakata N, Murakami T, Nakajima H, Nakadai. K. Wind-induced noise reduction by linear beamforming using a -channel microphone. The 8th Workshop on Circuits and Systems; 3-4 August 15; Himeji, Japan 15. p

3.2 Wind direction / wind velocity

3.2 Wind direction / wind velocity 3.2 Wind direction / wind velocity The direction from which air moves to is called the wind direction, and the distance air moves per unit time is the wind velocity. Wind has to be measured not only as

More information

Fan Stage Broadband Noise Benchmarking Programme

Fan Stage Broadband Noise Benchmarking Programme Fan Stage Broadband Noise Benchmarking Programme Specification of Fundamental Test Case 3 (FC3) Version 1 : 26 January 2015 Test Case Coordinator John Coupland ISVR University of Southampton UK E-mail

More information

Induced Electric Field

Induced Electric Field Lecture 18 Chapter 30 Physics II Induced Electric Field Course website: http://faculty.uml.edu/andriy_danylov/teaching/physicsii Today we are going to discuss: Chapter 30: Section 30.5, 30.6 Section 30.7

More information

Notes on Radian Measure

Notes on Radian Measure MAT 170 Pre-Calculus Notes on Radian Measure Radian Angles Terri L. Miller Spring 009 revised April 17, 009 1. Radian Measure Recall that a unit circle is the circle centered at the origin with a radius

More information

Induced Electric Field

Induced Electric Field Lecture 18 Chapter 33 Physics II Induced Electric Field Course website: http://faculty.uml.edu/andriy_danylov/teaching/physicsii Applications of Faraday s Law (some leftovers from the previous class) Applications

More information

Induced Electric Field

Induced Electric Field Lecture 20 Chapter 30 Induced Electric Field This fool said some nonsense that the electric field can be produced from the magnetic field. Course website: http://faculty.uml.edu/andriy_danylov/teaching/physicsii

More information

SOUND SOURCE LOCALIZATION VIA ELASTIC NET REGULARIZATION

SOUND SOURCE LOCALIZATION VIA ELASTIC NET REGULARIZATION BeBeC-2014-02 SOUND SOURCE LOCALIZATION VIA ELASTIC NET REGULARIZATION Xiaodong Li, Weiming Tong and Min Jiang School of Energy and Power engineering, Beihang University 100191, Beijing, China ABSTRACT

More information

Standard Practices for Air Speed Calibration Testing

Standard Practices for Air Speed Calibration Testing Standard Practices for Air Speed Calibration Testing Rachael V. Coquilla Bryza Wind Lab, Fairfield, California Air speed calibration is a test process where the output from a wind measuring instrument

More information

Department of Mechanical and Aerospace Engineering. MAE334 - Introduction to Instrumentation and Computers. Final Examination.

Department of Mechanical and Aerospace Engineering. MAE334 - Introduction to Instrumentation and Computers. Final Examination. Name: Number: Department of Mechanical and Aerospace Engineering MAE334 - Introduction to Instrumentation and Computers Final Examination December 12, 2003 Closed Book and Notes 1. Be sure to fill in your

More information

Modeling Measurement Uncertainty in Room Acoustics P. Dietrich

Modeling Measurement Uncertainty in Room Acoustics P. Dietrich Modeling Measurement Uncertainty in Room Acoustics P. Dietrich This paper investigates a way of determining and modeling uncertainty contributions in measurements of room acoustic parameters, which are

More information

Anemometry Anemometer Calibration Exercise

Anemometry Anemometer Calibration Exercise Atmospheric Measurements and Observations II EAS 535 Anemometry Anemometer Calibration Exercise Prof. J. Haase http://web.ics.purdue.edu/~jhaase/teaching/eas535/index.html Class Objectives How is wind

More information

APPLICATION OF MVDR BEAMFORMING TO SPHERICAL ARRAYS

APPLICATION OF MVDR BEAMFORMING TO SPHERICAL ARRAYS AMBISONICS SYMPOSIUM 29 June 2-27, Graz APPLICATION OF MVDR BEAMFORMING TO SPHERICAL ARRAYS Anton Schlesinger 1, Marinus M. Boone 2 1 University of Technology Delft, The Netherlands (a.schlesinger@tudelft.nl)

More information

19th European Signal Processing Conference (EUSIPCO 2011) Barcelona, Spain, August 29 - September 2, 2011

19th European Signal Processing Conference (EUSIPCO 2011) Barcelona, Spain, August 29 - September 2, 2011 19th European Signal Processing Conference (EUSIPCO 211) Barcelona, Spain, August 29 - September 2, 211 DEVELOPMENT OF PROTOTYPE SOUND DIRECTION CONTROL SYSTEM USING A TWO-DIMENSIONAL LOUDSPEAKER ARRAY

More information

Review of Anemometer Calibration Standards

Review of Anemometer Calibration Standards Review of Anemometer Calibration Standards Rachael V. Coquilla rvcoquilla@otechwind.com Otech Engineering, Inc., Davis, CA Anemometer calibration defines a relationship between the measured signals from

More information

An angle in the Cartesian plane is in standard position if its vertex lies at the origin and its initial arm lies on the positive x-axis.

An angle in the Cartesian plane is in standard position if its vertex lies at the origin and its initial arm lies on the positive x-axis. Learning Goals 1. To understand what standard position represents. 2. To understand what a principal and related acute angle are. 3. To understand that positive angles are measured by a counter-clockwise

More information

SONIC THERMOMETRY TODAY. W.R. Dagle and H.A. Zimmerman. Applied Technologies, Inc., Longmont, CO 80501

SONIC THERMOMETRY TODAY. W.R. Dagle and H.A. Zimmerman. Applied Technologies, Inc., Longmont, CO 80501 SONI THERMOMETRY TODAY W.R. Dagle and H.A. Zimmerman Applied Technologies, Inc., Longmont, O 80501 Sonic anemometer-thermometers began appearing in field studies over 50 years ago. They have since been

More information

A LOCALIZATION METHOD FOR MULTIPLE SOUND SOURCES BY USING COHERENCE FUNCTION

A LOCALIZATION METHOD FOR MULTIPLE SOUND SOURCES BY USING COHERENCE FUNCTION 8th European Signal Processing Conference (EUSIPCO-2) Aalborg, Denmark, August 23-27, 2 A LOCALIZATION METHOD FOR MULTIPLE SOUND SOURCES BY USING COHERENCE FUNCTION Hiromichi NAKASHIMA, Mitsuru KAWAMOTO,

More information

PHYSICS ADMISSIONS TEST SAMPLE PAPER (2015 style, issued September 2015) Time allowed: 2 hours

PHYSICS ADMISSIONS TEST SAMPLE PAPER (2015 style, issued September 2015) Time allowed: 2 hours PHYSICS ADMISSIONS TEST SAMPLE PAPER (2015 style, issued September 2015) Time allowed: 2 hours For candidates applying to Physics, Physics and Philosophy, Engineering, or Materials There are two Sections

More information

Sensing and Sensors: Fundamental Concepts

Sensing and Sensors: Fundamental Concepts Sensing and Sensors: Fundamental Concepts 2015 Sensitivity Range Precision Accuracy Resolution Offset Hysteresis Response Time Source: sensorwebs.jpl.nasa.gov Human Physiology in Space" by Barbara F. Abuja

More information

Aerodynamic noise produced in flow around an automobile bonnet

Aerodynamic noise produced in flow around an automobile bonnet Aerodynamic noise produced in flow around an automobile bonnet Hiroshi Yokoyama 1, Takahiro Nakajima 2, Taishi Shinohara 3, Masashi Miyazawa 4 and Akiyoshi Iida 5 1,2,3,5 Department of Mechanical Engineering,

More information

The Hilbert Transform

The Hilbert Transform The Hilbert Transform David Hilbert 1 ABSTRACT: In this presentation, the basic theoretical background of the Hilbert Transform is introduced. Using this transform, normal real-valued time domain functions

More information

THE HYDROFLOWN: MEMS-BASED UNDERWATER ACOUSTICAL PARTICLE VELOCITY SENSOR THE SENSOR, ITS CALIBRATION AND SOME POSSIBLE LOCALIZATION TECHNIQUES

THE HYDROFLOWN: MEMS-BASED UNDERWATER ACOUSTICAL PARTICLE VELOCITY SENSOR THE SENSOR, ITS CALIBRATION AND SOME POSSIBLE LOCALIZATION TECHNIQUES THE HYDROFLOWN: MEMS-BASED UNDERWATER ACOUSTICAL PARTICLE VELOCITY SENSOR THE SENSOR, ITS CALIBRATION AND SOME POSSIBLE LOCALIZATION TECHNIQUES Hans-Elias de Bree a, Berke M. Gur b, Tuncay Akal c a Microflown

More information

Effects of screens set characteristics on the flow field in a wind tunnel.

Effects of screens set characteristics on the flow field in a wind tunnel. Effects of screens set characteristics on the flow field in a wind tunnel. A M Santos, D B Souza, F O Costa, M H Farias, S Araújo, Y B Zanirath National Institute of Metrology, Quality and Technology Inmetro

More information

Trigonometry.notebook. March 16, Trigonometry. hypotenuse opposite. Recall: adjacent

Trigonometry.notebook. March 16, Trigonometry. hypotenuse opposite. Recall: adjacent Trigonometry Recall: hypotenuse opposite adjacent 1 There are 3 other ratios: the reciprocals of sine, cosine and tangent. Secant: Cosecant: (cosec θ) Cotangent: 2 Example: Determine the value of x. a)

More information

DIRECTION ESTIMATION BASED ON SOUND INTENSITY VECTORS. Sakari Tervo

DIRECTION ESTIMATION BASED ON SOUND INTENSITY VECTORS. Sakari Tervo 7th European Signal Processing Conference (EUSIPCO 9) Glasgow, Scotland, August 4-8, 9 DIRECTION ESTIMATION BASED ON SOUND INTENSITY VECTORS Sakari Tervo Helsinki University of Technology Department of

More information

Application Note. Brüel & Kjær. Tyre Noise Measurement on a Moving Vehicle. Introduction. by Per Rasmussen and Svend Gade, Brüel & Kjær, Denmark

Application Note. Brüel & Kjær. Tyre Noise Measurement on a Moving Vehicle. Introduction. by Per Rasmussen and Svend Gade, Brüel & Kjær, Denmark Application Note Tyre Noise Measurement on a Moving Vehicle by Per Rasmussen and Svend Gade,, Denmar To obtain precise information about the noise radiation from tyres it is desirable to measure with the

More information

Noise generated from Louver exposed to Flow and Countermeasure s Effect

Noise generated from Louver exposed to Flow and Countermeasure s Effect Noise generated from Louver exposed to Flow and Countermeasure s Effect Kunihiko Ishihara Abstract This paper describes effects of configuration of the louver and the long hole on aerodynamic noise level.

More information

EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE (V_3)

EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE (V_3) TA name Lab section Date TA Initials (on completion) Name UW Student ID # Lab Partner(s) EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE (V_3) 121 Textbook Reference: Knight, Chapter 13.1-3, 6. SYNOPSIS In

More information

Determination of the location of a sound source in 3D based on acoustic vector sensors on the ground

Determination of the location of a sound source in 3D based on acoustic vector sensors on the ground Baltimore, Maryland NOISE-CON 21 21 April 19-21 Determination of the location of a sound source in 3D based on acoustic vector sensors on the ground Antonio iñares, Erik Druyvesteyn, Jelmer Wind, Hans-Elias

More information

PROPAGATION PHASE REPRESENTATION IN 3D SPACE USING POLES AND ZEROS IN COMPLEX FREQUENCY PLANE. ( address of lead author)

PROPAGATION PHASE REPRESENTATION IN 3D SPACE USING POLES AND ZEROS IN COMPLEX FREQUENCY PLANE. ( address of lead author) ICSV14 Cairns Australia 9-12 July, 2007 PROPAGATION PHASE REPRESENTATION IN 3D SPACE USING POLES AND ZEROS IN COMPLEX FREQUENCY PLANE Yoshinori Takahashi 1, Mikio Tohyama 2, and Kazunori Miyoshi 1 1 Kogakuin

More information

Highly resolved turbulence budgets over a desert playa

Highly resolved turbulence budgets over a desert playa Highly resolved turbulence budgets over a desert playa Vigneshwaran Kulandaivelu Derek Jenson & Eric Pardyjak Department of Mechanical Engineering University of Utah Gilad Arwatz & Marcus Hultmark Princeton

More information

1. Trigonometry.notebook. September 29, Trigonometry. hypotenuse opposite. Recall: adjacent

1. Trigonometry.notebook. September 29, Trigonometry. hypotenuse opposite. Recall: adjacent Trigonometry Recall: hypotenuse opposite adjacent 1 There are 3 other ratios: the reciprocals of sine, cosine and tangent. Secant: Cosecant: (cosec θ) Cotangent: 2 Example: Determine the value of x. a)

More information

Sound Source Tracking Using Microphone Arrays

Sound Source Tracking Using Microphone Arrays Sound Source Tracking Using Microphone Arrays WANG PENG and WEE SER Center for Signal Processing School of Electrical & Electronic Engineering Nanayang Technological Univerisy SINGAPORE, 639798 Abstract:

More information

Development of PC-Based Leak Detection System Using Acoustic Emission Technique

Development of PC-Based Leak Detection System Using Acoustic Emission Technique Key Engineering Materials Online: 004-08-5 ISSN: 66-9795, Vols. 70-7, pp 55-50 doi:0.408/www.scientific.net/kem.70-7.55 004 Trans Tech Publications, Switzerland Citation & Copyright (to be inserted by

More information

USA Mathematical Talent Search Round 1 Solutions Year 24 Academic Year

USA Mathematical Talent Search Round 1 Solutions Year 24 Academic Year 1/1/24. Several children were playing in the ugly tree when suddenly they all fell. Roger hit branches A, B, and C in that order on the way down. Sue hit branches D, E, and F in that order on the way down.

More information

Acoustics Laboratory

Acoustics Laboratory Acoustics Laboratory 1 at the Center for Noise and Vibration Control in ME, KAIST Supervisor: Prof. Jeong-Guon Ih (e-mail: J.G.Ih@kaist.ac.kr) Lab members: (as of March 2015) Ph.D. Students: 6 (1 part-time

More information

Maxim > Design Support > Technical Documents > Application Notes > Wireless and RF > APP 1851

Maxim > Design Support > Technical Documents > Application Notes > Wireless and RF > APP 1851 Maxim > Design Support > Technical Documents > Application Notes > Wireless and RF > APP 1851 Keywords: lna, rf, rfic, amplifier, stability, power gain, transmission lines, rfics, theory, smith chart,

More information

The definition of the coordinate system indicating sensor positions is shown in Figure 1. +V Vertical. -Y Left side along the driving direction

The definition of the coordinate system indicating sensor positions is shown in Figure 1. +V Vertical. -Y Left side along the driving direction 1 Standardisation of test method for salt spreader: Air flow experiments Report 5: Three dimensional velocity and its components by Hisamitsu Takai and Jan S. Strøm, Consultants Aarhus University, Engineering

More information

On the correlation of the acoustic signal of microphones mounted on a flat plate to the turbulence of an impinging jet

On the correlation of the acoustic signal of microphones mounted on a flat plate to the turbulence of an impinging jet On the correlation of the acoustic signal of microphones mounted on a flat plate to the turbulence of an impinging jet C. Reichl a, M. Boeck a, W. Tilser a, H. Lang a, K. Haindl b, F. Reining b and M.

More information

International Journal of Advanced Research in Computer Science and Software Engineering

International Journal of Advanced Research in Computer Science and Software Engineering Volume 2, Issue 11, November 2012 ISSN: 2277 128X International Journal of Advanced Research in Computer Science and Software Engineering Research Paper Available online at: www.ijarcsse.com Acoustic Source

More information

Compensator Design to Improve Transient Performance Using Root Locus

Compensator Design to Improve Transient Performance Using Root Locus 1 Compensator Design to Improve Transient Performance Using Root Locus Prof. Guy Beale Electrical and Computer Engineering Department George Mason University Fairfax, Virginia Correspondence concerning

More information

Cepstral Deconvolution Method for Measurement of Absorption and Scattering Coefficients of Materials

Cepstral Deconvolution Method for Measurement of Absorption and Scattering Coefficients of Materials Cepstral Deconvolution Method for Measurement of Absorption and Scattering Coefficients of Materials Mehmet ÇALIŞKAN a) Middle East Technical University, Department of Mechanical Engineering, Ankara, 06800,

More information

Analysis of Flow inside Soundproofing Ventilation Unit using CFD

Analysis of Flow inside Soundproofing Ventilation Unit using CFD International Journal of Emerging Engineering Research and Technology Volume 6, Issue 8, 2018, PP 1-8 ISSN 2349-4395 (Print) & ISSN 2349-4409 (Online) Analysis of Flow inside Soundproofing Ventilation

More information

2d-Laser Cantilever Anemometer

2d-Laser Cantilever Anemometer 2d-Laser Cantilever Anemometer Introduction Measuring principle Calibration Design Comparative measurement Contact: Jaroslaw Puczylowski University of Oldenburg jaroslaw.puczylowski@forwind.de Introduction

More information

Cross-spectral Matrix Diagonal Reconstruction

Cross-spectral Matrix Diagonal Reconstruction Cross-spectral Matrix Diagonal Reconstruction Jørgen HALD 1 1 Brüel & Kjær SVM A/S, Denmark ABSTRACT In some cases, measured cross-spectral matrices (CSM s) from a microphone array will be contaminated

More information

Using this definition, it is possible to define an angle of any (positive or negative) measurement by recognizing how its terminal side is obtained.

Using this definition, it is possible to define an angle of any (positive or negative) measurement by recognizing how its terminal side is obtained. Angle in Standard Position With the Cartesian plane, we define an angle in Standard Position if it has its vertex on the origin and one of its sides ( called the initial side ) is always on the positive

More information

NOISE ROBUST RELATIVE TRANSFER FUNCTION ESTIMATION. M. Schwab, P. Noll, and T. Sikora. Technical University Berlin, Germany Communication System Group

NOISE ROBUST RELATIVE TRANSFER FUNCTION ESTIMATION. M. Schwab, P. Noll, and T. Sikora. Technical University Berlin, Germany Communication System Group NOISE ROBUST RELATIVE TRANSFER FUNCTION ESTIMATION M. Schwab, P. Noll, and T. Sikora Technical University Berlin, Germany Communication System Group Einsteinufer 17, 1557 Berlin (Germany) {schwab noll

More information

EFFECTS OF ACOUSTIC SCATTERING AT ROUGH SURFACES ON THE

EFFECTS OF ACOUSTIC SCATTERING AT ROUGH SURFACES ON THE EFFECTS OF ACOUSTIC SCATTERING AT ROUGH SURFACES ON THE SENSITIVITY OF ULTRASONIC INSPECTION Peter B. Nagy and Laszlo Adler Department of Welding Engineering The Ohio State University Columbus, Ohio 4321

More information

Lecture Notes 1: Vector spaces

Lecture Notes 1: Vector spaces Optimization-based data analysis Fall 2017 Lecture Notes 1: Vector spaces In this chapter we review certain basic concepts of linear algebra, highlighting their application to signal processing. 1 Vector

More information

Turbulence Measurements with the Upgraded Phase Contrast Imaging Diagnostic in Alcator C-Mod

Turbulence Measurements with the Upgraded Phase Contrast Imaging Diagnostic in Alcator C-Mod Turbulence Measurements with the Upgraded Phase Contrast Imaging Diagnostic in L. Lin, M. Porkolab, E. M. Edlund, Y. Lin, S. J. Wukitch Plasma Science and Fusion Center, MIT, Cambridge, MA, 02139 48 th

More information

Chapter 3. Vectors and Two-Dimensional Motion

Chapter 3. Vectors and Two-Dimensional Motion Chapter 3 Vectors and Two-Dimensional Motion 1 Vector vs. Scalar Review All physical quantities encountered in this text will be either a scalar or a vector A vector quantity has both magnitude (size)

More information

Lecture 6 - Introduction to Electricity

Lecture 6 - Introduction to Electricity Lecture 6 - Introduction to Electricity A Puzzle... We are all familiar with visualizing an integral as the area under a curve. For example, a b f[x] dx equals the sum of the areas of the rectangles of

More information

Study on the Performance of a Sirocco Fan (Flow Around the Runner Blade)

Study on the Performance of a Sirocco Fan (Flow Around the Runner Blade) Rotating Machinery, 10(5): 415 424, 2004 Copyright c Taylor & Francis Inc. ISSN: 1023-621X print / 1542-3034 online DOI: 10.1080/10236210490474629 Study on the Performance of a Sirocco Fan (Flow Around

More information

Acoustic holography. LMS Test.Lab. Rev 12A

Acoustic holography. LMS Test.Lab. Rev 12A Acoustic holography LMS Test.Lab Rev 12A Copyright LMS International 2012 Table of Contents Chapter 1 Introduction... 5 Chapter 2... 7 Section 2.1 Temporal and spatial frequency... 7 Section 2.2 Time

More information

Numerical sound field analysis considering atmospheric conditions

Numerical sound field analysis considering atmospheric conditions Numerical sound field analysis considering atmospheric conditions Satoshi Ogawa 1 and Yasuhiro Oikawa 2 1,2 Department of Intermedia Art and Science, Waseda University 3-4-1 Okubo, Shinjuku-ku, Tokyo 169-8555,

More information

MICROPHONE ARRAY METHOD FOR THE CHARACTERIZATION OF ROTATING SOUND SOURCES IN AXIAL FANS

MICROPHONE ARRAY METHOD FOR THE CHARACTERIZATION OF ROTATING SOUND SOURCES IN AXIAL FANS MICROPHONE ARRAY METHOD FOR THE CHARACTERIZATION OF ROTATING SOUND SOURCES IN AXIAL FANS Gert HEROLD, Ennes SARRADJ Brandenburg University of Technology, Chair of Technical Acoustics, Siemens-Halske-Ring

More information

NIHON. Experimental and Computational Study of Boundary Layer Transition by Two-Dimensional Roughness (January 1997) NIHON

NIHON. Experimental and Computational Study of Boundary Layer Transition by Two-Dimensional Roughness (January 1997) NIHON ardekani@irost.ir NIHON Experimental and Computational Study of Boundary Layer Transition by Two-Dimensional Roughness (January 1997) NIHON The Mechanism of Boundary Layer Transition by Two-Dimensional

More information

Lab Partner(s) TA Initials (on completion) EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE

Lab Partner(s) TA Initials (on completion) EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE TA name Lab section Date TA Initials (on completion) Name UW Student ID # Lab Partner(s) EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE 117 Textbook Reference: Walker, Chapter 10-1,2, Chapter 11-1,3 SYNOPSIS

More information

Indicate whether each statement is true or false by circling your answer. No explanation for your choice is required. Each answer is worth 3 points.

Indicate whether each statement is true or false by circling your answer. No explanation for your choice is required. Each answer is worth 3 points. Physics 5B FINAL EXAM Winter 2009 PART I (15 points): True/False Indicate whether each statement is true or false by circling your answer. No explanation for your choice is required. Each answer is worth

More information

Fluctuating Pressure Inside/Outside the Flow Separation Region in High Speed Flowfield

Fluctuating Pressure Inside/Outside the Flow Separation Region in High Speed Flowfield Journal of Aerospace Science and Technology 1 (2015) 18-26 doi: 10.17265/2332-8258/2015.01.003 D DAVID PUBLISHING Fluctuating Pressure Inside/Outside the Flow Separation Region in High Speed Flowfield

More information

Signal Modeling Techniques in Speech Recognition. Hassan A. Kingravi

Signal Modeling Techniques in Speech Recognition. Hassan A. Kingravi Signal Modeling Techniques in Speech Recognition Hassan A. Kingravi Outline Introduction Spectral Shaping Spectral Analysis Parameter Transforms Statistical Modeling Discussion Conclusions 1: Introduction

More information

An Observer for Phased Microphone Array Signal Processing with Nonlinear Output

An Observer for Phased Microphone Array Signal Processing with Nonlinear Output 2010 Asia-Pacific International Symposium on Aerospace Technology An Observer for Phased Microphone Array Signal Processing with Nonlinear Output Bai Long 1,*, Huang Xun 2 1 Department of Mechanics and

More information

SUPPLEMENTARY FIGURES

SUPPLEMENTARY FIGURES SUPPLEMENTARY FIGURES Supplementary Figure 1. Projected band structures for different coupling strengths. (a) The non-dispersive quasi-energy diagrams and (b) projected band structures for constant coupling

More information

Bayesian Optimization

Bayesian Optimization Practitioner Course: Portfolio October 15, 2008 No introduction to portfolio optimization would be complete without acknowledging the significant contribution of the Markowitz mean-variance efficient frontier

More information

Coefficients of Recursive Linear Time-Invariant First-Order Low-Pass and High-Pass Filters (v0.1)

Coefficients of Recursive Linear Time-Invariant First-Order Low-Pass and High-Pass Filters (v0.1) Coefficients of Recursive Linear Time-Invariant First-Order Low-Pass and High-Pass Filters (v0. Cliff Sparks www.arpchord.com The following is a quick overview of recursive linear time-invariant first-order

More information

Solutions of a PT-symmetric Dimer with Constant Gain-loss

Solutions of a PT-symmetric Dimer with Constant Gain-loss Solutions of a PT-symmetric Dimer with Constant Gain-loss G14DIS Mathematics 4th Year Dissertation Spring 2012/2013 School of Mathematical Sciences University of Nottingham John Pickton Supervisor: Dr

More information

Research Article The Microphone Feedback Analogy for Chatter in Machining

Research Article The Microphone Feedback Analogy for Chatter in Machining Shock and Vibration Volume 215, Article ID 976819, 5 pages http://dx.doi.org/1.1155/215/976819 Research Article The Microphone Feedback Analogy for Chatter in Machining Tony Schmitz UniversityofNorthCarolinaatCharlotte,Charlotte,NC28223,USA

More information

Advanced Signal Processing on Temperature Sensor Arrays for Fire Location Estimation

Advanced Signal Processing on Temperature Sensor Arrays for Fire Location Estimation Martin Berentsen 1, Thomas Kaiser 1, Shu Wang 2 1: Fachgebiet Nachrichtentechnische Systeme, Institut für Nachrichten- u. Kommunikationstechnik, Fakultät für Ingenieurwissenschaften, Universität Duisburg-Essen,

More information

Estimating Correlation Coefficient Between Two Complex Signals Without Phase Observation

Estimating Correlation Coefficient Between Two Complex Signals Without Phase Observation Estimating Correlation Coefficient Between Two Complex Signals Without Phase Observation Shigeki Miyabe 1B, Notubaka Ono 2, and Shoji Makino 1 1 University of Tsukuba, 1-1-1 Tennodai, Tsukuba, Ibaraki

More information

MockTime.com. (b) 9/2 (c) 18 (d) 27

MockTime.com. (b) 9/2 (c) 18 (d) 27 212 NDA Mathematics Practice Set 1. Let X be any non-empty set containing n elements. Then what is the number of relations on X? 2 n 2 2n 2 2n n 2 2. Only 1 2 and 3 1 and 2 1 and 3 3. Consider the following

More information

19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, 2-7 SEPTEMBER 2007

19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, 2-7 SEPTEMBER 2007 19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, -7 SEPTEMBER 007 Numerical simulation of low level sonic boom propagation through random inhomogeneous sound speed fields PACS: 43.8.Mw Ollivier, Sébastien

More information

A) I B) II C) III D) IV E) V

A) I B) II C) III D) IV E) V 1. A square loop of wire moves with a constant speed v from a field-free region into a region of uniform B field, as shown. Which of the five graphs correctly shows the induced current i in the loop as

More information

Adaptive beamforming. Slide 2: Chapter 7: Adaptive array processing. Slide 3: Delay-and-sum. Slide 4: Delay-and-sum, continued

Adaptive beamforming. Slide 2: Chapter 7: Adaptive array processing. Slide 3: Delay-and-sum. Slide 4: Delay-and-sum, continued INF540 202 Adaptive beamforming p Adaptive beamforming Sven Peter Näsholm Department of Informatics, University of Oslo Spring semester 202 svenpn@ifiuiono Office phone number: +47 22840068 Slide 2: Chapter

More information

NIH Public Access Author Manuscript Ultrason Imaging. Author manuscript; available in PMC 2013 November 21.

NIH Public Access Author Manuscript Ultrason Imaging. Author manuscript; available in PMC 2013 November 21. NIH Public Access Author Manuscript Published in final edited form as: Ultrason Imaging. 2012 October ; 34(4):. doi:10.1177/0161734612463847. Rapid Transient Pressure Field Computations in the Nearfield

More information

2. Find the side lengths of a square whose diagonal is length State the side ratios of the special right triangles, and

2. Find the side lengths of a square whose diagonal is length State the side ratios of the special right triangles, and 1. Starting at the same spot on a circular track that is 80 meters in diameter, Hayley and Kendall run in opposite directions, at 300 meters per minute and 240 meters per minute, respectively. They run

More information

Exam 2, Phy 2049, Spring Solutions:

Exam 2, Phy 2049, Spring Solutions: Exam 2, Phy 2049, Spring 2017. Solutions: 1. A battery, which has an emf of EMF = 10V and an internal resistance of R 0 = 50Ω, is connected to three resistors, as shown in the figure. The resistors have

More information

Profs. Y. Takano, P. Avery, S. Hershfield. Final Exam Solution

Profs. Y. Takano, P. Avery, S. Hershfield. Final Exam Solution PHY2049 Fall 2008 Profs. Y. Takano, P. Avery, S. Hershfield Final Exam Solution Note that each problem has three versions, each with different numbers and answers (separated by ). The numbers for each

More information

Symmetries 2 - Rotations in Space

Symmetries 2 - Rotations in Space Symmetries 2 - Rotations in Space This symmetry is about the isotropy of space, i.e. space is the same in all orientations. Thus, if we continuously rotated an entire system in space, we expect the system

More information

Course End Review Grade 10: Academic Mathematics

Course End Review Grade 10: Academic Mathematics Course End Review Grade 10: Academic Mathematics Linear Systems: 1. For each of the following linear equations place in y = mx + b format. (a) 3 x + 6y = 1 (b) 4 x 3y = 15. Given 1 x 4y = 36, state: (a)

More information

Well resolved measurements of turbulent fluxes in the atmospheric surface layer

Well resolved measurements of turbulent fluxes in the atmospheric surface layer Well resolved measurements of turbulent fluxes in the atmospheric surface layer M. Hultmark, G. Arwatz, M. Vallikivi, Y. Fan and C. Bahri Princeton University Department of Mechanical and Aerospace Engineering

More information

Experimental approach on natural frequency of window vibration induced by low frequency sounds

Experimental approach on natural frequency of window vibration induced by low frequency sounds INTER-NOISE 216 Experimental approach on natural frequency of window vibration induced by low frequency sounds Tetsuya DOI 1 ; Keiichiro IWANAGA 1 ; Michiko JIMBO 2 1 Kobayasi Institute of Physical Research,

More information

Calculation of spatial sound intensity distribution based on synchronised measurement of acoustic pressure

Calculation of spatial sound intensity distribution based on synchronised measurement of acoustic pressure Calculation of spatial sound intensity distribution based on synchronised measurement of acoustic pressure Witold Mickiewicz, Michał Jakub Jabłoński West Pomeranian University of Technology Szczecin Faculty

More information

3 Severe Weather. Critical Thinking

3 Severe Weather. Critical Thinking CHAPTER 2 3 Severe Weather SECTION Understanding Weather BEFORE YOU READ After you read this section, you should be able to answer these questions: What are some types of severe weather? How can you stay

More information

Complex Terrain (EDUCT) experiment, conducted by the National Center for Atmospheric

Complex Terrain (EDUCT) experiment, conducted by the National Center for Atmospheric Alex Ameen Shenandoah Trip Paper I visited Shenandoah National Park on April 11, 2009 to investigate the Education in Complex Terrain (EDUCT) experiment, conducted by the National Center for Atmospheric

More information

Mathematics 5 SN TRIGONOMETRY PROBLEMS 2., which one of the following statements is TRUE?, which one of the following statements is TRUE?

Mathematics 5 SN TRIGONOMETRY PROBLEMS 2., which one of the following statements is TRUE?, which one of the following statements is TRUE? Mathematics 5 SN TRIGONOMETRY PROBLEMS 1 If x 4 which one of the following statements is TRUE? A) sin x > 0 and cos x > 0 C) sin x < 0 and cos x > 0 B) sin x > 0 and cos x < 0 D) sin x < 0 and cos x

More information

1.1 Find the measures of two angles, one positive and one negative, that are coterminal with the given angle. 1) 162

1.1 Find the measures of two angles, one positive and one negative, that are coterminal with the given angle. 1) 162 Math 00 Midterm Review Dugopolski Trigonometr Edition, Chapter and. Find the measures of two angles, one positive and one negative, that are coterminal with the given angle. ) ) - ) For the given angle,

More information

Technical Explanation for Axial Fans

Technical Explanation for Axial Fans CSM_Axial_TG_E Introduction What Is an Axial? Axial fans are used for stable cooling in many different applications and locations. If the temperature of a device increases, the lives of its internal parts

More information

Control Systems. Frequency Method Nyquist Analysis.

Control Systems. Frequency Method Nyquist Analysis. Frequency Method Nyquist Analysis chibum@seoultech.ac.kr Outline Polar plots Nyquist plots Factors of polar plots PolarNyquist Plots Polar plot: he locus of the magnitude of ω vs. the phase of ω on polar

More information

ON THE NOISE REDUCTION PERFORMANCE OF THE MVDR BEAMFORMER IN NOISY AND REVERBERANT ENVIRONMENTS

ON THE NOISE REDUCTION PERFORMANCE OF THE MVDR BEAMFORMER IN NOISY AND REVERBERANT ENVIRONMENTS 0 IEEE International Conference on Acoustic, Speech and Signal Processing (ICASSP) ON THE NOISE REDUCTION PERFORANCE OF THE VDR BEAFORER IN NOISY AND REVERBERANT ENVIRONENTS Chao Pan, Jingdong Chen, and

More information

MTH 122: Section 204. Plane Trigonometry. Test 1

MTH 122: Section 204. Plane Trigonometry. Test 1 MTH 122: Section 204. Plane Trigonometry. Test 1 Section A: No use of calculator is allowed. Show your work and clearly identify your answer. 1. a). Complete the following table. α 0 π/6 π/4 π/3 π/2 π

More information

Verification of contribution separation technique for vehicle interior noise using only response signals

Verification of contribution separation technique for vehicle interior noise using only response signals Verification of contribution separation technique for vehicle interior noise using only response signals Tomohiro HIRANO 1 ; Junji YOSHIDA 1 1 Osaka Institute of Technology, Japan ABSTRACT In this study,

More information

Piezoelectric sensing and actuation CEE575

Piezoelectric sensing and actuation CEE575 Piezoelectric sensing and actuation CEE575 Sensor: Mechanical energy to electrical energy Actuator: Electrical energy converted to mechanical energy (motion) Materials For many years, natural crystals

More information

674 JVE INTERNATIONAL LTD. JOURNAL OF VIBROENGINEERING. MAR 2015, VOLUME 17, ISSUE 2. ISSN

674 JVE INTERNATIONAL LTD. JOURNAL OF VIBROENGINEERING. MAR 2015, VOLUME 17, ISSUE 2. ISSN 1545. The improved separation method of coherent sources with two measurement surfaces based on statistically optimized near-field acoustical holography Jin Mao 1, Zhongming Xu 2, Zhifei Zhang 3, Yansong

More information

Math 1720 Final Exam REVIEW Show All work!

Math 1720 Final Exam REVIEW Show All work! Math 1720 Final Exam REVIEW Show All work! The Final Exam will contain problems/questions that fit into these Course Outcomes (stated on the course syllabus): Upon completion of this course, students will:

More information

Final Exam Review Packet

Final Exam Review Packet Final Exam Review Packet Multiple Choice Identify the choice that best completes the statement or answers the question. 1. Find the length of the missing side. The triangle is not drawn to scale. 6 8 a.

More information

Shankar Shivappa University of California, San Diego April 26, CSE 254 Seminar in learning algorithms

Shankar Shivappa University of California, San Diego April 26, CSE 254 Seminar in learning algorithms Recognition of Visual Speech Elements Using Adaptively Boosted Hidden Markov Models. Say Wei Foo, Yong Lian, Liang Dong. IEEE Transactions on Circuits and Systems for Video Technology, May 2004. Shankar

More information

2. (i) Find the equation of the circle which passes through ( 7, 1) and has centre ( 4, 3).

2. (i) Find the equation of the circle which passes through ( 7, 1) and has centre ( 4, 3). Circle 1. (i) Find the equation of the circle with centre ( 7, 3) and of radius 10. (ii) Find the centre of the circle 2x 2 + 2y 2 + 6x + 8y 1 = 0 (iii) What is the radius of the circle 3x 2 + 3y 2 + 5x

More information

HiSPARC Detector - Detector Station

HiSPARC Detector - Detector Station HiSPARC Detector - Detector Station Koos Kortland translated and adapted by K. Schadenberg 1 Introduction This module is a part of a series describing the HiSPARC detector. A detector station consists

More information

Automatic time picking and velocity determination on full waveform sonic well logs

Automatic time picking and velocity determination on full waveform sonic well logs Automatic time picking and velocity determination on full waveform sonic well logs Lejia Han, Joe Wong, John C. Bancroft, and Robert R. Stewart ABSTRACT Full waveform sonic logging is used to determine

More information

Exercise. Exercise 1.1. MA112 Section : Prepared by Dr.Archara Pacheenburawana 1

Exercise. Exercise 1.1. MA112 Section : Prepared by Dr.Archara Pacheenburawana 1 MA112 Section 750001: Prepared by Dr.Archara Pacheenburawana 1 Exercise Exercise 1.1 1 8 Find the vertex, focus, and directrix of the parabola and sketch its graph. 1. x = 2y 2 2. 4y +x 2 = 0 3. 4x 2 =

More information