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Learjet Acoustics Flight Test – An Initial Look The motivation for the work is the need for an improved ability to predict takeoff noise of future commercial supersonic aircraft. The overall objective is to validate as well as improve the conversion of facility scale-model data and semi-empirical jet-noise predictions to flight noise. As a first step, the processing of data and results from an acoustics flight test are described. The next step involves the comparison of the flight acoustic data and complementary rig-test results. This will be presented in future reports. Ultimately, the goal is improved noise-prediction methods for system studies of future commercial supersonic aircraft.
Document ID
20230003135
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Lennart S. Hultgren
(Glenn Research Center Cleveland, Ohio, United States)
Brenda S. Henderson
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
March 8, 2023
Subject Category
Aeronautics (General)
Meeting Information
Meeting: NASA Acoustics Technical Working Group
Location: Hampton, VA
Country: US
Start Date: March 21, 2023
End Date: March 22, 2023
Sponsors: Acoustics Technical Working Group
Funding Number(s)
WBS: 110076.02.03.04.40.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
aeroacoustics, jet noise, flyover noise
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