Background Noise Levels Measured in the NASA Lewis 9-by 15-foot Low-speed Wind Tunnel

Background Noise Levels Measured in the NASA Lewis 9-by 15-foot Low-speed Wind Tunnel PDF Author: Richard P. Woodward
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 14

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Background Noise Levels Measured in the NASA Lewis 9-by 15-foot Low-speed Wind Tunnel

Background Noise Levels Measured in the NASA Lewis 9-by 15-foot Low-speed Wind Tunnel PDF Author: Richard P. Woodward
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 14

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Acoustical Evaluation of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel

Acoustical Evaluation of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel PDF Author: Milo D. Dahl
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 68

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Noise Measurements from an Ejector Suppressor Nozzle in the NASA Lewis 9- by 15-foot Low Speed Wind Tunnel

Noise Measurements from an Ejector Suppressor Nozzle in the NASA Lewis 9- by 15-foot Low Speed Wind Tunnel PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Acoustical Evaluation of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel

Acoustical Evaluation of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722155667
Category :
Languages : en
Pages : 64

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Book Description
The test section of the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel was acoustically treated to allow the measurement of acoustic sources located within the tunnel test section under simulated free field conditions. The treatment was designed for high sound absorption at frequencies above 250 Hz and to withstand tunnel airflow velocities up to 0.2 Mach. Evaluation tests with no tunnel airflow were conducted in the test section to assess the performance of the installed treatment. This performance would not be significantly affected by low speed airflow. Time delay spectrometry tests showed that interference ripples in the incident signal resulting from reflections occurring within the test section average from 1.7 dB to 3.2 dB wide over a 500 to 5150 Hz frequency range. Late reflections, from upstream and downstream of the test section, were found to be insignificant at the microphone measuring points. For acoustic sources with low directivity characteristics, decay with distance measurements in the test section showed that incident free field behavior can be measured on average with an accuracy of +/- 1.5 dB or better at source frequencies from 400 Hz to 10 kHz. The free field variations are typically much smaller with an omnidirectional source. Dahl, Milo D. and Woodward, Richard P. Glenn Research Center...

Calibration of the NASA Lewis Research Center 9- by 15-Foot Low Speed Wind Tunnel (1994 Test)

Calibration of the NASA Lewis Research Center 9- by 15-Foot Low Speed Wind Tunnel (1994 Test) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 190

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 372

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NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548

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STAR

STAR PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 904

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Aeroacoustic Measurements

Aeroacoustic Measurements PDF Author: Thomas J. Mueller
Publisher: Springer Science & Business Media
ISBN: 3662050587
Category : Technology & Engineering
Languages : en
Pages : 327

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Book Description
The book describes recent developments in aeroacoustic measurements in wind tunnels and the interpretation of the resulting data. The reader will find the latest measurement techniques described along with examples of the results.