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Mach Cutoff Analysis and Results from NASA's Farfield Investigation of No-Boom ThresholdsIn support of the ongoing effort by the National Aeronautics and Space Administration (NASA) to bring supersonic commercial travel to the public, the NASA Armstrong Flight Research Center and the NASA Langley Research Center,in partnership with other industry organizations and academia, conducted a flight research experiment to analyze acoustic propagation in the Mach cutoff shadow zone. The effort was conducted in fall of 2012 and named the Farfield Investigation of No-boom Thresholds (FaINT). The test helped to build a data set that will go toward further understanding of the unique acoustic propagation characteristics below Mach cutoff altitude.
Document ID
20160007349
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Cliatt, Larry J., II
(NASA Dryden Flight Research Center Edwards, CA United States)
Hill, Michael A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Haering, Edward A, Jr.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
June 8, 2016
Publication Date
June 1, 2016
Subject Category
Aircraft Design, Testing And Performance
Acoustics
Aerodynamics
Report/Patent Number
DFRC-E-DAA-TN32472
Report Number: DFRC-E-DAA-TN32472
Meeting Information
Meeting: Industry Panel Presentation at the University of Southern California
Location: Los Angeles, CA
Country: United States
Start Date: November 3, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, University of Southern California
Funding Number(s)
WBS: WBS 110076.02.02.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
sonic boom
acoustics
flight research
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