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  • 2015-2019  (2)
  • 2010-2014  (1)
  • 2015  (2)
  • 2012  (1)
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  • 2015-2019  (2)
  • 2010-2014  (1)
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  • 1
    Publication Date: 2019-07-13
    Description: Successful execution of the flight phase of the Superboom Caustic Analysis and Measurement Project (SCAMP) required accurate placement of focused sonic booms on an array of prepositioned ground sensors. While the array was spread over a 10,000-ft-long area, this is a relatively small region when considering the speed of a supersonic aircraft and sonic boom ray path variability due to shifting atmospheric conditions and aircraft trajectories. Another requirement of the project was to determine the proper position for a microphone-equipped motorized glider to intercept the sonic boom caustic, adding critical timing to the constraints. Variability in several inputs to these calculations caused some shifts of the focus away from the optimal location. Reports of the sonic booms heard by persons positioned amongst the array were used to shift the focus closer to the optimal location for subsequent passes. This paper describes the methods and computations used to place the focused sonic boom on the SCAMP array and gives recommendations for their accurate placement by future quiet supersonic aircraft. For the SCAMP flights, 67% of the foci were placed on the ground array with measured positions within a few thousand feet of computed positions. Among those foci with large caustic elevation angles, 96% of foci were placed on the array, and measured positions were within a few hundred feet of computed positions. The motorized glider captured sonic booms on 59% of the passes when the instrumentation was operating properly.
    Keywords: Acoustics
    Type: DFRC-E-DAA-TN6916 , AIAA Aerospace Sciences Meeting; Dec 19, 2012 - Dec 21, 2012; Grapevine, TX; United States|Industry Panel Presentation at the University of Southern California; Nov 03, 2017; Los Angeles, CA; United States
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  • 2
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Aerodynamics; Acoustics
    Type: AFRC-E-DAA-TN24565 , International Symposium on Nonlinear Acoustics; Jun 29, 2015 - Jul 03, 2015; Lyon; France|International Sonic Boom Forum; Jul 02, 2015 - Jul 03, 2015; Lyon; France|Industry Panel Presentation at the University of Southern California; Nov 03, 2017; Los Angeles, CA; United States
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  • 3
    Publication Date: 2019-07-13
    Description: In support of the ongoing effort by the National Aeronautics and Space Administration (NASA) to bring supersonic commercial travel to the public, NASA, in partnership with other industry organizations, conducted a flight research experiment to analyze acoustic propagation at the lateral edge of the sonic boom carpet. The name of the effort was the Farfield Investigation of No-boom Thresholds (FaINT). The research from FaINT determined an appropriate metric for sonic boom waveforms in the transition and shadow zones called Perceived Sound Exposure Level, established a value of 65 dB as a limit for the acoustic lateral extent of a sonic boom's noise region, analyzed change in sonic boom levels near lateral cutoff, and compared between real sonic boom measurements and numerical predictions.
    Keywords: Acoustics; Aerodynamics
    Type: AFRC-E-DAA-TN23247 , International Symposium on NonLinear Acoustics; Jun 29, 2015 - Jul 03, 2015; Lyon; France
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