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Effects of simulated forward flight on jet noise, shock noise and internal noiseInflight simulation experiments are conducted in an anechoic free-jet facility to examine the flight effects on various combinations of jet noise, shock noise and internal noise. The jet mixing noise component reduces with forward velocity at all angles and frequencies. When jet mixing noise is contaminated with internal noise, forward motion provides a noise reduction in the rear arc and a noise increase in the forward arc, with little change at 90 deg. The results are similar for shock-containing jets. It is found that the existing anomalies between full-scale flight data and model-scale flight simulation data could well be due to the contamination of the flight data by internal noise.
Document ID
19790042923
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ahuja, K. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Tanna, H. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Tester, B. J.
(Lockheed-Georgia Co. Marietta, Ga., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 79-0615
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aeroacoustics Conference
Location: Seattle, WA
Start Date: March 12, 1979
End Date: March 14, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A26936
Funding Number(s)
CONTRACT_GRANT: NAS3-20050
Distribution Limits
Public
Copyright
Other

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