NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The free jet as a simulator of forward velocity effects on jet noiseA thorough theoretical and experimental study of the effects of the free-jet shear layer on the transmission of sound from a model jet placed within the free jet to the far-field receiver located outside the free-jet flow was conducted. The validity and accuracy of the free-jet flight simulation technique for forward velocity effects on jet noise was evaluated. Transformation charts and a systematic computational procedure for converting measurements from a free-jet simulation to the corresponding results from a wind-tunnel simulation, and, finally, to the flight case were provided. The effects of simulated forward flight on jet mixing noise, internal noise and shock-associated noise from model-scale unheated and heated jets were established experimentally in a free-jet facility. It was illustrated that the existing anomalies between full-scale flight data and model-scale flight simulation data projected to the flight case, could well be due to the contamination of flight data by engine internal noise.
Document ID
19790006702
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ahuja, K. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Tester, B. J.
(Lockheed-Georgia Co. Marietta, GA, United States)
Tanna, H. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Acoustics
Report/Patent Number
NASA-CR-3056
LG78ER0065
Report Number: NASA-CR-3056
Report Number: LG78ER0065
Accession Number
79N14873
Funding Number(s)
CONTRACT_GRANT: NAS3-20050
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available