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Sonic Boom Prediction and Mitigation using Three-Dimensional Earth EffectsAs the industry progresses towards realizing a commercial supersonic aircraft, the push to reduce noise from sonic boom has intensified. This emphasizes the need to better understand and accurately model the underlying physics and seek ways to reduce modeling gaps in the calculation of sonic boom noise metrics. To answer this need, sonic boom prediction capability of the atmospheric propagation tool sBOOM is enhanced to include three-dimensional Earth effects during propagation. The discrete adjoint capability under three-dimensional effects is also enhanced to be helpful in design optimization. The differences in ground signatures, noise metrics, and carpet widths are compared against results obtained using flat Earth approximation and discussed. Finally, the developed capability is used in CFD based shape optimization to demonstrate the differences in aircraft outer mold line when ellipsoidal Earth effects during shape optimization for sonic boom mitigation.
Document ID
20190000992
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Rallabhandi, Sriram K.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 27, 2019
Publication Date
June 25, 2018
Subject Category
Computer Programming And Software
Aircraft Design, Testing And Performance
Acoustics
Report/Patent Number
NF1676L-28587
Report Number: NF1676L-28587
Meeting Information
Meeting: AIAA Aviation Forum
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: WBS 110076.02.07.03.12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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