Publikationsdatum:
2019-07-13
Beschreibung:
The 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.
Schlagwort(e):
Aircraft Design, Testing and Performance
Materialart:
AFRC-E-DAA-TN43652
,
Industry Panel Presentation at the University of Southern California; Nov 03, 2017; Los Angeles, CA; United States|Acoustics 2017; Jun 25, 2017 - Jun 29, 2017; Boston, MA; United States
Format:
application/pdf
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