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Sonic Booms in Atmospheric Turbulence (SonicBAT) Ground Measurements in a Hot Desert ClimateThe Sonic Booms in Atmospheric Turbulence (SonicBAT) Project flew a series of 20 F-18 flights with 69 supersonic passes at Edwards Air Force Base in July 2016 to quantify the effect of atmospheric turbulence on sonic booms. Most of the passes were at a pressure altitude of 32,000 feet and a Mach number of 1.4, yielding a nominal sonic boom overpressure of 1.6 pounds per square foot. Atmospheric sensors such as GPS sondeballoons, Sonic Detection and Ranging (SODAR) acoustic sounders, and ultrasonic anemometers were used to characterize the turbulence state of the atmosphere for each flight. Spiked signatures in excess of 7 pounds per square foot were measured at some locations, as well as rounded sonic-boom signatures with levels much lower than the nominal. This presentation will quantify the range of overpressure and Perceived Level of the sonic boom as a function of turbulence parameters, and also present the spatial variation of these quantities over the array. Comparison with historical data will also be shown.
Document ID
20170006088
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Haering, Edward A., Jr.
(NASA Armstrong Flight Research Center Edwards, CA United States)
Date Acquired
July 6, 2017
Publication Date
June 27, 2017
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AFRC-E-DAA-TN43652
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: University of Southern California, Acoustical Society of America
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
acoustic testing
sonic booms
ground testing
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