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5 TABLE OF ONTENTS MULTIPLE LOATION QUALIFIATION... i LIST OF TABLES... iv LIST OF FIGURES... iv LIST OF SYMBOLS...v TEST RESULTS...1 TEST DESRIPTION INTRODUTION TEST DESRIPTION Flat Plate Elimination Test Measurements alibration and Acceptance riteria TEST RESULTS Test Presentation alculation of the alibration and Acceptance riteria Flat Plate Elimination Tests REFERENES ATTAHMENT ATTAHMENT AREDITATION FP iii

6 LIST OF TABLES Table 1 - Fluid Identification... 3 Table 2 - Apparent Surface Tension, ph and Refractive Index... 3 Table 3 - Brookfield Viscosity (mpa s)... 5 Table 4 - Aerodynamic Performance Test Data: 71/29 Dilution... 7 Table 5 - Aerodynamic Performance Test Data: 50/50 Dilution... 9 Table 6 - Refractive Index Data and Water hange: 71/29 Dilution Table 7 - Refractive Index Data and Water hange: 50/50 Dilution Table 8 - Viscosity Measurement Details Table 9 - Dry Test Data Table 10 - Aerodynamic Performance Test Data : Reference Fluid Table 11 - Refractive Index Data and Water hange: Reference Fluid LIST OF FIGURES Figure 1 - Aerodynamic Test Results Figure 2 - Fluid Elimination Figure 3 - Relative Humidity Figure 4 - Refractive Index versus Water ontent Figure 5 - FPET Set-up Figure 6 - Take-off Ground Acceleration Simulation Figure 7 - Acceptance riteria FP iv

7 LIST OF SYMBOLS * ave average Boundary Layer Displacement Thickness (BLDT) over the test section perimeter at cross-section 3 (Figure 5) evaluated by the equation 2 in Attachment 1 (mm) * Boundary Layer Displacement Thickness (BLDT) over the test section perimeter at cross-section 3 (Figure 5) evaluated by the equation 3 in Attachment 1 (mm) AIR Aerospave Information Report AMIL Anti-icing Materials International Laboratory AMS Aerospace Material Specification AS Aerospace Standard FE Fluid Elimination during the test (%) FP Flat Plate elimination test identification number FP Flat Plate alibration test identification number FPD Flat Plate elimination test Dry (without fluid) FPET Flat Plate Elimination Test P Static Pressure as measured by gauges positioned at points # 1, 2 and 3 in the set-up (Figure 5) (mpa) Rh Relative humidity (%) SAE Society of Automotive Engineers t T a T f UQA V W Thickness of the film fluid on the plate ( m) Air Temperature as recorded at the top of the cross-section 2 in the set up (Figure 5) ( ) Fluid Temperature as recorded in the fluid film at the bottom of the cross-section 3 (Figure 5) ( ) University of Quebec at hicoutimi Air Velocity derived from the measurement of the pressure difference P 1 - P 2 using the equation (1) Attachment 1 (m/s) Water hange (% w/w) FP v

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9 TEST RESULTS FP

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11 Table 1 - Fluid Identification ompany Name Product AMIL Label olor Manuf. Location Manuf. Date Recep. Date ABAX INDUSTRIES IN. DE-950 Lot # L NEAT DE-950 Lot # L /29 J579 Orange FRed & Holmberg & o in Kalmar, Sweden J DE-950 Lot # L /50 J581 AMIL Reference Fluid * lot # /25 M127 olorless Saguenay, Quebec (anada) Table 2 - Apparent Surface Tension, ph and Refractive Index DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L Apparent Surface Tension (± 0.5) ph (± 0.1) Refractive Index (± ) Fluid T dynes/cm T Value T Value J J M127-1 NOT REQUIRED * For the reference fluid formulation, refer to AS5900B paragraph for the low speed ramp tests. FP

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13 Table 3 - Brookfield Viscosity (mpa s) DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L Fluid Temp ( ) 0.3 RPM 6 RPM 30 RPM Viscosity Accuracy Spindle # Viscosity Accuracy Spindle # Viscosity Accuracy Spindle # J < J < < M < For additional viscosity details, see Table 8. FP

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15 Table 4 - Aerodynamic Performance Test Data: 71/29 Dilution TEST ODE DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L LOW SPEED RAMP T a T f Rh % T o (1) m T end (2) m FE (3) % W (4) % V (5) m/s * mm J580A * J580A * J580A * J J J J580E J580E J580E J580F J580F J580F J580F J580F *caution : value outside the ±2% range Acceptance riteria : (1) (2) (3) (4) (5 D -20 = mm (1) Thickness of the fluid measured at the beginning of the test. (2) Thickness of the fluid measured at the end of the test. (3) Fluid Elimination. (4) Water hange. (5) Air velocity 30 seconds after the beginning of the test. FP

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17 Table 5 - Aerodynamic Performance Test Data: 50/50 Dilution TEST ODE DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L LOW SPEED RAMP T a T f Rh % T o (1) m T end (2) m FE (3) % W (4) % V (5) m/s * mm J581A * J581A * J581A * J J J J581E J581E J581E *caution : value outside the ±2% range Acceptance riteria : (1) (2) (3) (4) ( D -20 = mm (1) Thickness of the fluid measured at the beginning of the test. (2) Thickness of the fluid measured at the end of the test. (3) Fluid Elimination. (4) Water hange. (5) Air velocity 30 seconds after the beginning of the test. FP

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19 Figure 1 - Aerodynamic Test Results FP

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21 Figure 2 - Fluid Elimination FP

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23 Figure 3 - Relative Humidity FP

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25 Table 6 - Refractive Index Data and Water hange: 71/29 Dilution DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L TEST ODE RI Initial RI Final RI W % W/W RH % J580A * 88.5 J580A * 86.8 J580A * 87.0 J J J J580E J580E J580E J580F J580F J580F J580F J580F *caution : value outside the ±2% range Table 7 - Refractive Index Data and Water hange: 50/50 Dilution DEIING FLUID ABAX INDUSTRIES IN. DE-950, lot # L TEST ODE RI Initial RI Final RI W % W/W RH % J581A * 89.0 J581A * 88.3 J581A * 88.6 J J J J581E J581E J581E *caution : value outside the ±2% range FP

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27 REFRATIVE INDEX FLUID ONENTRATION (% w/w) M127 J580 J581 M127: RI = % w/w J580 : RI = % w/w J581 : RI = % w/w BASIS : 100% w/w corresponds to NEAT fluid Figure 4 - Refractive Index versus Water ontent FP

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29 TEST DESRIPTION FP

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31 1. INTRODUTION This report details the performance of fluid samples, identified in Table 1, when subjected to the Flat Plate Elimination Test, denoted FPET hereafter. The FPET procedure follows the SAE Aerospace Material Specifications, AMS 1424K [2] and AS5900B [3] for deicing fluid on the low-speed ramp. The tests were carried out in the Luan Phan refrigerated wind tunnel of the "Anti-icing Materials International Laboratory" (AMIL) at the "Université du Québec à hicoutimi" (UQA) [4]. UQA facility is operated independently from fluid manufacturers and meets the requirements of the aerodynamic acceptance testing standards. It was found qualified on September 11, 1997 (reconfirmed September 13 th, 2012) by the Performance Review institute according to PRI document A3001, audit criteria for compliance to SAE AMS1424 and AMS TEST DESRIPTION 2.1 Flat Plate Elimination Test This test is designed to measure the Boundary Layer Displacement Thickness, BLDT, which is related to lift loss [5]. The flat plate set-up consists of a duct inserted in the test section of AMIL cold wind tunnel. In this tunnel, the airflow and the fluid can be maintained at a constant temperature, between 5 ± 1 and 45 ± 2. A set-up sketch is given in Figure 5. The FPET procedure consists in submitting a 2 mm thick layer of deicing product covering the duct floor to an accelerating air flow of 2.1 m/s², simulating a low take-off rotation speed commuter type aircraft (Figure 6). The BLDT on the flat plate is measured at pressure tap location # 3 (Figure 5), twenty seconds after the beginning of the simulated take-off. A detailed description of this test is presented in AS5900B [3]. FP

32 Air Velocity (m/s) Figure 5 - FPET Set-up 50 Low Speed Ramp m/s ± 3 m/s sec ± Time (s) Figure 6 - Take-off Ground Acceleration Simulation FP

33 2.2 Measurements In a FPET, the fluid performance is evaluated from BLDT measurements. The BLDT value used for the fluid evaluation is the average of the BLDT measured between the 19th and the 21st seconds after the beginning of the test. The starting time (t = 0) is evaluated by extrapolating the straight line of the acceleration ramp to the point where V = 0 m/s. In addition, the following parameters are measured: 1. apparent surface tension at room temperature (dynes/cm) Apparent Surface Tension measured with a DuNouy precision tensiometer, S Scientific ompany Inc., model No , using a cm pulling ring. 2. ph at room temperature ph values measured with a Fisher Accumet phmeter, Fisher Scientific ompany, model 925, using a phresh, Flow-On-Demand Epoxy Body ombination ph Electrode, Beckman, model refractive index which is used to determine the water change (%) Refractive Index measured with a REIHERT AR7 SERIES Refractometer, Reichert, Inc., model AR viscosity at room and test temperatures (mpa s) 5. fluid film thickness ( m) at the beginning and at the end of the FPET to compute fluid elimination (%) FP

34 Table 8 - Viscosity Measurement Details Fluid Type I II III IV Measurement Device LV SSA Spindle # ontainer Description Sample Rotation Duration (min) Volume (ml) 0.3 RPM 6 RPM 30 RPM ml Beaker R (P) R (P) R (P) R (P) The viscometers are calibrated yearly by the accredited laboratory AN-AM Instruments, Ltd. The NIST traceable calibration certificate is available upon request. 2.3 alibration and Acceptance riteria The calibration is obtained from dry tests, performed without fluid, and Reference Fluid tests (as described in AS5900B paragraph 2.1.4), for which BLDT results are well documented. The BLDT values obtained from a dry test should be 2.8 mm ± 0.4 mm. For dry and calibration tests, the BLDT values are recorded at four temperatures: 0, -10, -20 and -25. Reference Fluid BLDT values and dry BLDT values are used to calculate the acceptance criteria required for certification. A candidate fluid is acceptable at a test temperature if none of the independent BLDT measurements is greater than the acceptance criteria. This test temperature is the average of the three lowest temperatures of the acceptable data points. 3. TEST RESULTS 3.1 Test Presentation The fluid identification is presented in Table 1 and the fluid physical properties in the following tables : Apparent surface tension, ph and refractive index values are given in Table 2 and Brookfield viscosity values in Table 3. FPET results are presented in Table 4 and Table 5. alibration data from dry tests and tests with the Reference Fluid are reproduced in Table 9 and Table 10 respectively. Finally, FP

35 Table 6 and Table 7 present refractive index data and water change calculations. Figure 4 shows the refractive index as a function of water change. Fluid elimination and relative humidity are presented as a function of test temperature in Figure 2 and Figure 3 respectively. 3.2 alculation of the alibration and Acceptance riteria alibration tests, as defined in section 2.3, consist of dry tests and tests with the Reference Fluid. The dry test results are presented in Table 9. According to specifications [2], the AMIL system is considered adequately calibrated, since the dry test BLDT value( *) varies within the standard range of 2.8 mm ± 0.4 mm. The Reference Fluid results are presented in Table 10. These results are also in agreement with known values. As mentioned in section 2.3, dry and Reference Fluid BLDT values are used to compute the criteria of acceptance, presented below and in Figure 7. The acceptance envelope is a constant straight line with a BLDT equal to the value D20. The D20 is calculated accordingly to the AS5900B [3] for the low take-off rotation speed ramp: alculation of acceptance level at -20 : D * * * 20 ( ) ref ref dry 20 D20 = ( ) x ( ) = mm FP

36 Table 9 - Dry Test Data TEST ODE T a T f Rh(%) V (1) (m/s) * dry (mm) DRY_A DRY_A DRY_A DRY_A DRY_ DRY_ DRY_ DRY_ DRY_E DRY_E DRY_E DRY_E DRY_F DRY_F DRY_F DRY_F (1 (1) Air velocity 30 seconds after the beginning of the test FP

37 (1) (2) (3) (4) ( Table 10 - Aerodynamic Performance Test Data : Reference Fluid TEST ODE T a T f Rh % T o (1) m T end (2) m FE (3) % W (4) % V (5) m/s * mm M127A * M127A * M127A * M M M M127E M127E M127E M127F M127F M127F *caution : value outside the ±2% range (1) Thickness of the fluid measured at the beginning of the test. (2) Thickness of the fluid measured at the end of the test. (3) Fluid Elimination. (4) Water hange. (5) Air velocity 30 seconds after the beginning of the test. FP

38 Table 11 - Refractive Index Data and Water hange: Reference Fluid TEST ODE RI Initial RI Final RI W % W/W RH % M127A * 83.3 M127A * 82.4 M127A * 87.3 M M M M127E M127E M127E M127F M127F M127F *caution : value outside the ±2% range FP

39 Figure 7 - Acceptance riteria FP

40 3.3 Flat Plate Elimination Tests BLDT, fluid elimination and water change values are listed in Table 4 and Table 5 for each test. In Figure 1, BLDT values are presented in comparison with the acceptance criteria. This figure shows that the candidate fluid ABAX INDUSTRIES IN. DE-950 lot # L is acceptable with the low speed ramp above in the case of the 71/29 dilution, and above -20 in the case of the 50/50 dilution. 4. REFERENES 1. American Society for Testing and Materials "Standard Specification for Reagent Water", ASTM D , SAE International Aerospace Material Specification, "Deicing/Anti-icing Fluid, Aircraft, SAE Type I", AMS 1424, revision K, March SAE International Aerospace Standard, "Standard Test Method for Aerodynamic Acceptance of SAE AMS 1424 and SAE AMS 1428 Aircraft Deicing/Anti-icing Fluids", AS5900, revision B, July 1, Laforte, J.-L., P. Louchez, G. Bouchard, and M. Farzaneh, "A Facility to Evaluate Performance of Aircraft Ground De/Anti-Icing Fluids Subjected to Freezing Rain". old Regions Science and Technology, : p Laforte, J.-L., P. Louchez, and G. Bouchard, "Experimental Evaluation of Flat Plate Boundary Layer Growth over an Anti-Icing Fluid Film". anadian Aeronautics and Space Journal, (2): p FP

41 ATTAHMENT 1 Measurement Principle * The time varying velocity at the inlet of the test section will be derived from the measurement of the pressure difference P1 - P2, recorded as a function of time during all test runs. For such purpose, the following relation, obtained from application of Bernouilli and continuity equations according to usual wind tunnel practice, will be used: V P P S S 1 (1) where is the mass per unit volume of the test gas at the test conditions, and S1/S2 is the area ratio of the wind tunnel contraction. The boundary layer displacement thickness (BLDT) on the bottom flat plate, at the location of the pressure tap P3 (cross-section 3), will be evaluated from the measurement of the two pressure differences P1 - P2 and P1 - P3 recorded as functions of time during all the test runs. Indeed, an increase in BLDT from inlet to outlet of the test section causes a restriction of the net cross-sectional area, thus producing an increase in the air velocity along the test section, which in turn causes a decrease of static pressure from cross-section 2 to 3. * This text reproduces Appendix B of DOUMENT NO D : "Aerodynamic Acceptance Test for Aircraft Ground Deicing/Anti-icing Fluids". BOEING ommercial Airplane ompany. FP

42 * More precisely, the average BLDT ave over the test section perimeter, at crosssection 3, will be evaluated using following relation, obtained from application of mass conservation and Bernouilli equations: 1 ave c S S P P * P P P P (2) where c is the test section perimeter at cross-section 3, and S2 and S3 are the areas of cross-sections 2 and 3 respectively. When no fluid is present on the bottom flat plate, all four test section walls are in the same dry state, and the previous expression (2) yields the value of the BLDT on a dry wall: (with no fluid) * * dry ave On the other hand, when the bottom plate of the test section is covered with a layer of de/anti-icing fluid, and the top and sides are not, the BLDT is not constant over the perimeter of the cross-section 3. Indeed, it assumes a value * on the bottom plate and another value on the sides and top wall. Expressing the previously * * determined ave as a perimeter-weighted average of dry and *, the following relation can be obtained: c c b ave b c * * * dry (3) where b is the width of the bottom flat plate. This relation will be used to derive * the BLDT over a wet surface, *, from the measurement of ave carried out as explained with fluid on the bottom test section wall, provided an expression for FP

43 * dry has been previously determined by a number of "dry" runs, carried out without any fluid in the test section. More precisely, these dry runs, to be made during the * setting up and calibration of the facility, will yield the value of dry and they will be used to determine the constant in the following empirical formula: * dry V const n 1 5 (4) where V is the tunnel air velocity at cross-section 2 and n is the cinematic viscosity of the test gas at the test conditions. For data reduction of a test with fluid in the test section, this last expression (4) will be used to evaluate, as * function of the instantaneous velocity determined by (1), the value of dry to be used in expression (3). FP

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45 ATTAHMENT 2 TEST DATA SHEETS 1 DRY RUNS RUNS WITH REFERENE FLUID M DE-950 lot # L14-042, 71/29 Dilution J DE-950 lot # L14-042, 50/50 Dilution J FP

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47 1 DRY RUNS FP

48 DRY_A L.P.wind tunnel AMIL :25 Slope : 1.90 m/s 2 TEST RUN DATA Test : DRY_A277 Rh avg = 86.5 % At 20 sec: V = 35.1 m/s T a avg = -0.6 o T f avg = 0.6 o * dry = 2.88 mm V (m/s) time (sec) -T f (mm) ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

49 DRY_A L.P.wind tunnel AMIL :39 Slope : 1.95 m/s 2 TEST RUN DATA Test : DRY_A278 Rh avg = 84.4 % At 20 sec: V = 35.0 m/s T a avg = -0.6 o T f avg = 0.1 o * dry = 2.91 mm V (m/s) time (sec) -T f (mm) ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

50 DRY_A L.P.wind tunnel AMIL :22 Slope : 1.92 m/s 2 TEST RUN DATA Test : DRY_A279 Rh avg = 84.7 % At 20 sec: V = 35.0 m/s T a avg = -0.8 o T f avg = -0.1 o * dry = 2.89 mm V (m/s) time (sec) -T f (mm) ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

51 DRY_A L.P.wind tunnel AMIL :06 Slope : 1.93 m/s 2 TEST RUN DATA Test : DRY_A280 Rh avg = 91.0 % At 20 sec: V = 35.1 m/s T a avg = -0.6 o T f avg = -0.2 o * dry = 2.86 mm V (m/s) time (sec) -T f (mm) ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

52 DRY_ L.P.wind tunnel AMIL :25 Slope : 1.96 m/s 2 TEST RUN DATA Test : DRY_281 Rh avg = 82.1 % At 20 sec: V = 35.2 m/s T a avg = o T f avg = o * dry = 2.91 mm V (m/s) T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

53 DRY_ L.P.wind tunnel AMIL :43 Slope : 1.95 m/s 2 TEST RUN DATA Test : DRY_282 Rh avg = 78.4 % At 20 sec: V = 35.1 m/s T a avg = o T f avg = o * dry = 2.91 mm V (m/s) T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

54 DRY_ L.P.wind tunnel AMIL :33 Slope : 2.02 m/s 2 TEST RUN DATA Test : DRY_283 Rh avg = 83.8 % At 20 sec: V = 35.1 m/s T a avg = o T f avg = o * dry = 2.91 mm V (m/s) T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

55 DRY_ L.P.wind tunnel AMIL :15 Slope : 2.02 m/s 2 TEST RUN DATA Test : DRY_284 Rh avg = 83.1 % At 20 sec: V = 33.3 m/s T a avg = o T f avg = o * dry = 2.90 mm V (m/s) T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

56 DRY_E L.P.wind tunnel AMIL :28 Slope : 2.03 m/s 2 TEST RUN DATA Test : DRY_E285 Rh avg = 61.3 % At 20 sec: V = 35.2 m/s T a avg = o T f avg = o * dry = 2.98 mm V (m/s) 20 -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

57 DRY_E L.P.wind tunnel AMIL :47 Slope : 1.95 m/s 2 TEST RUN DATA Test : DRY_E286 Rh avg = 62.1 % At 20 sec: V = 35.1 m/s T a avg = o T f avg = o * dry = 2.98 mm V (m/s) 20 -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

58 DRY_E L.P.wind tunnel AMIL :39 Slope : 1.95 m/s 2 TEST RUN DATA Test : DRY_E287 Rh avg = 65.5 % At 20 sec: V = 34.9 m/s T a avg = o T f avg = o * dry = 2.96 mm V (m/s) 20 -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

59 DRY_E L.P.wind tunnel AMIL :29 Slope : 1.93 m/s 2 TEST RUN DATA Test : DRY_E289 Rh avg = 67.1 % At 20 sec: V = 35.1 m/s T a avg = o T f avg = o * dry = 2.99 mm V (m/s) 20 -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

60 DRY_F L.P.wind tunnel AMIL :22 Slope : 1.99 m/s 2 TEST RUN DATA Test : DRY_F290 Rh avg = 65.8 % At 20 sec: V = 35.0 m/s T a avg = o T f avg = o * dry = 3.00 mm V (m/s) -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

61 DRY_F L.P.wind tunnel AMIL :42 Slope : 2.03 m/s 2 TEST RUN DATA Test : DRY_F291 Rh avg = 65.0 % At 20 sec: V = 35.0 m/s T a avg = o T f avg = o * dry = 3.00 mm V (m/s) -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

62 DRY_F L.P.wind tunnel AMIL :54 Slope : 1.97 m/s 2 TEST RUN DATA Test : DRY_F292 Rh avg = 64.2 % At 20 sec: V = 34.5 m/s T a avg = o T f avg = o * dry = 3.04 mm V (m/s) -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

63 DRY_F L.P.wind tunnel AMIL :11 Slope : 1.96 m/s 2 TEST RUN DATA Test : DRY_F298 Rh avg = 65.8 % At 20 sec: V = 34.9 m/s T a avg = o T f avg = o * dry = 3.08 mm V (m/s) -T f ( o ) time (sec) (mm) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 * Sec o o % "H 2 O m/s "H 2 O mm Averages: Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm FP

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65 2 RUNS WITH REFERENE FLUID M127 FP

66 M127A L.P.wind tunnel AMIL :29 Slope : 1.67 m/s 2 TEST RUN DATA Test : M127A369 Rh avg = 84.0 % At 20 sec: V = 35.8 m/s T a avg = -0.7 o T f avg = -0.1 o dry = 2.85 mm = 6.68 mm max = mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

67 M127A L.P.wind tunnel AMIL :35 Slope : 1.68 m/s 2 TEST RUN DATA Test : M127A370 Rh avg = 83.4 % At 20 sec: V = 35.1 m/s T a avg = -0.8 o T f avg = -0.4 o dry = 2.85 mm = 6.70 mm max = mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

68 M127A L.P.wind tunnel AMIL :19 Slope : 1.68 m/s 2 TEST RUN DATA Test : M127A371 Rh avg = 87.8 % At 20 sec: V = 36.4 m/s T a avg = -0.4 o T f avg = -0.8 o dry = 2.85 mm = 6.85 mm max = mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

69 M L.P.wind tunnel AMIL :32 Slope : 1.72 m/s 2 TEST RUN DATA Test : M Rh avg = 79.7 % At 20 sec: V = 36.1 m/s T a avg = o T f avg = o dry = 2.85 mm = 8.28 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

70 M L.P.wind tunnel AMIL :39 Slope : 1.69 m/s 2 TEST RUN DATA Test : M Rh avg = 81.6 % At 20 sec: V = 35.0 m/s T a avg = o T f avg = o dry = 2.85 mm = 8.59 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

71 M L.P.wind tunnel AMIL :28 Slope : 1.71 m/s 2 TEST RUN DATA Test : M Rh avg = 79.5 % At 20 sec: V = 36.2 m/s T a avg = o T f avg = o dry = 2.85 mm = 8.27 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

72 M127E L.P.wind tunnel AMIL :34 Slope : 1.70 m/s 2 TEST RUN DATA Test : M127E375 Rh avg = 58.0 % At 20 sec: V = 34.3 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

73 M127E L.P.wind tunnel AMIL :43 Slope : 1.63 m/s 2 TEST RUN DATA Test : M127E376 Rh avg = 58.4 % At 20 sec: V = 34.8 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

74 M127E L.P.wind tunnel AMIL :35 Slope : 1.69 m/s 2 TEST RUN DATA Test : M127E377 Rh avg = 62.1 % At 20 sec: V = 33.6 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

75 M127F L.P.wind tunnel AMIL :31 Slope : 1.69 m/s 2 TEST RUN DATA Test : M127F378 Rh avg = 61.8 % At 20 sec: V = 34.1 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

76 M127F L.P.wind tunnel AMIL :38 Slope : 1.72 m/s 2 TEST RUN DATA Test : M127F379 Rh avg = 62.8 % At 20 sec: V = 34.1 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

77 M127F L.P.wind tunnel AMIL :50 Slope : 1.71 m/s 2 TEST RUN DATA Test : M127F380 Rh avg = 61.0 % At 20 sec: V = 34.3 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

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79 ABAX INDUSTRIES IN. DEIING FLUID 3 DE-950 lot # L14-042, 71/29 Dilution J-580 FP

80 J580A L.P.wind tunnel AMIL :26 Slope : 1.60 m/s 2 TEST RUN DATA Test : J580A850 Rh avg = 87.5 % At 20 sec: V = 35.7 m/s T a avg = -0.7 o T f avg = -0.8 o dry = 2.85 mm = 5.95 mm max = mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

81 J580A L.P.wind tunnel AMIL :33 Slope : 1.64 m/s 2 TEST RUN DATA Test : J580A851 Rh avg = 87.7 % At 20 sec: V = 35.5 m/s T a avg = -0.7 o T f avg = -0.8 o dry = 2.85 mm = 5.62 mm max = 9.81 mm at t = 5.90 sec V (m/s) time (sec) -T (mm) f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

82 J580A L.P.wind tunnel AMIL :40 Slope : 1.67 m/s 2 TEST RUN DATA Test : J580A852 Rh avg = 89.2 % At 20 sec: V = 35.7 m/s T a avg = -0.5 o T f avg = -0.5 o dry = 2.85 mm = 5.90 mm max = 9.65 mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

83 J L.P.wind tunnel AMIL :39 Slope : 1.71 m/s 2 TEST RUN DATA Test : J Rh avg = 82.8 % At 20 sec: V = 36.7 m/s T a avg = o T f avg = o dry = 2.85 mm = 7.08 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

84 J L.P.wind tunnel AMIL :47 Slope : 1.78 m/s 2 TEST RUN DATA Test : J Rh avg = 84.2 % At 20 sec: V = 36.3 m/s T a avg = o T f avg = o dry = 2.85 mm = 6.95 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

85 J L.P.wind tunnel AMIL :52 Slope : 1.71 m/s 2 TEST RUN DATA Test : J Rh avg = 81.1 % At 20 sec: V = 35.8 m/s T a avg = o T f avg = o dry = 2.85 mm = 7.25 mm max = mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

86 J580E L.P.wind tunnel AMIL :46 Slope : 1.80 m/s 2 TEST RUN DATA Test : J580E874 Rh avg = 64.6 % At 20 sec: V = 36.8 m/s T a avg = o T f avg = o dry = 2.85 mm = 8.75 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

87 J580E L.P.wind tunnel AMIL :53 Slope : 1.79 m/s 2 TEST RUN DATA Test : J580E875 Rh avg = 62.1 % At 20 sec: V = 36.9 m/s T a avg = o T f avg = o dry = 2.85 mm = 9.11 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

88 J580E L.P.wind tunnel AMIL :09 Slope : 1.82 m/s 2 TEST RUN DATA Test : J580E876 Rh avg = 61.5 % At 20 sec: V = 36.9 m/s T a avg = o T f avg = o dry = 2.85 mm = 8.90 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

89 J580F L.P.wind tunnel AMIL :24 Slope : 1.79 m/s 2 TEST RUN DATA Test : J580F881 Rh avg = 59.0 % At 20 sec: V = 35.6 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

90 J580F L.P.wind tunnel AMIL :35 Slope : 1.82 m/s 2 TEST RUN DATA Test : J580F882 Rh avg = 63.8 % At 20 sec: V = 36.2 m/s T a avg = o T f avg = o dry = 2.85 mm = mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

91 J580F L.P.wind tunnel AMIL :49 Slope : 1.87 m/s 2 TEST RUN DATA Test : J580F883 Rh avg = 64.8 % At 20 sec: V = 36.7 m/s T a avg = o T f avg = o dry = 2.85 mm = 9.90 mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

92 J580F L.P.wind tunnel AMIL :58 Slope : 1.88 m/s 2 TEST RUN DATA Test : J580F884 Rh avg = 61.9 % At 20 sec: V = 36.4 m/s T a avg = o T f avg = o dry = 2.85 mm = 9.97 mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

93 J580F L.P.wind tunnel AMIL :08 Slope : 1.90 m/s 2 TEST RUN DATA Test : J580F885 Rh avg = 65.0 % At 20 sec: V = 36.4 m/s T a avg = o T f avg = o dry = 2.85 mm = 9.23 mm max = mm at t = 5.90 sec V (m/s) -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

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95 ABAX INDUSTRIES IN. DEIING FLUID 4 DE-950 lot # L14-042, 50/50 Dilution J-581 FP

96 L.P.wind tunnel AMIL :46 Slope : 1.66 m/s 2 J581A853 TEST RUN DATA Test : J581A853 Rh avg = 89.4 % At 20 sec: V = 36.3 m/s T a avg = -0.5 o T f avg = -0.6 o dry = 2.85 mm = 4.89 mm max = 8.76 mm at t = 5.90 sec V (m/s) time (sec) (mm) -T f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

97 L.P.wind tunnel AMIL :54 Slope : 1.65 m/s 2 J581A854 TEST RUN DATA Test : J581A854 Rh avg = 89.1 % At 20 sec: V = 36.1 m/s T a avg = -0.7 o T f avg = -0.8 o dry = 2.85 mm = 4.75 mm max = 7.65 mm at t = 5.90 sec V (m/s) time (sec) -T (mm) f ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

98 L.P.wind tunnel AMIL :01 Slope : 1.76 m/s 2 J581A855 TEST RUN DATA Test : J581A855 Rh avg = 89.2 % At 20 sec: V = 36.6 m/s T a avg = -0.7 o T f avg = -0.9 o dry = 2.85 mm = 4.68 mm max = 7.71 mm at t = 5.90 sec V (m/s) time (sec) -T f (mm) ( o ) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

99 L.P.wind tunnel AMIL :59 Slope : 1.77 m/s 2 J TEST RUN DATA Test : J Rh avg = 82.1 % At 20 sec: V = 36.2 m/s T a avg = o T f avg = o dry = 2.85 mm = 5.41 mm max = 9.82 mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

100 L.P.wind tunnel AMIL :07 Slope : 1.74 m/s 2 J TEST RUN DATA Test : J Rh avg = 83.5 % At 20 sec: V = 36.8 m/s T a avg = o T f avg = o dry = 2.85 mm = 5.27 mm max = 9.51 mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

101 L.P.wind tunnel AMIL :12 Slope : 1.78 m/s 2 J TEST RUN DATA Test : J Rh avg = 80.1 % At 20 sec: V = 36.4 m/s T a avg = o T f avg = o dry = 2.85 mm = 5.32 mm max = 9.89 mm at t = 5.90 sec V (m/s) T f ( o ) (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

102 L.P.wind tunnel AMIL :14 Slope : 1.74 m/s 2 J581E877 TEST RUN DATA Test : J581E877 Rh avg = 64.2 % At 20 sec: V = 36.9 m/s T a avg = o T f avg = o dry = 2.85 mm = 6.97 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

103 L.P.wind tunnel AMIL :19 Slope : 1.74 m/s 2 J581E878 TEST RUN DATA Test : J581E878 Rh avg = 63.6 % At 20 sec: V = 37.1 m/s T a avg = o T f avg = o dry = 2.85 mm = 6.96 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 0 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

104 L.P.wind tunnel AMIL :26 Slope : 1.79 m/s 2 J581E879 TEST RUN DATA Test : J581E879 Rh avg = 65.2 % At 20 sec: V = 36.8 m/s T a avg = o T f avg = o dry = 2.85 mm = 6.73 mm max = mm at t = 5.90 sec V (m/s) 20 -T f ( o ) 10 (mm) time (sec) U.Q.A.. RITIAL TIME TEST DATA time T a T f Rh P 1 -P 2 V P 2 -P 3 Sec o o % "H 2 O m/s "H 2 O mm Averages : Test Duct Dimensions : S2 = mm² S3 = mm² B3 = mm 3 = mm² FP

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