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Atmospheric effects on the risetime and waveshape of sonic boomsAccurate prediction of human response to sonic booms from proposed HSCT aircraft depends on a knowledge of the waveshape and risetime of the boom at the ground. In previous work, we have developed a numerical technique to predict the combined effects of molecular absorption and finite wave distortion on the sonic boom as it propagates from the aircraft to the top of the turbulent boundary layer. We have more recently developed a scattering center based model to calculate the effects of turbulence on the sonic boom waveform as it propagates through this boundary layer. Calculations have been performed using single scales of turbulence and compared to measurements at Edwards AFB in the late 1960's. A model of the atmosphere involving two scales each for convective and mechanical turbulence has been developed and fit to meteorological data collected during JAPE 2. Scattering calculations employing this model underpredict the number of unperturbed waveforms. In order to develop a more realistic model of the atmosphere, the JAPE 2 meteorological data has been fit to a von Karman spectrum. Results of scattering using this multi-scale model will be presented. The combination of finite wave effects with turbulent scattering predictions includes the principal effects of the atmosphere on the sonic boom from the HSCT.
Document ID
19950008472
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raspet, Richard
(Mississippi Univ. University, MS, United States)
Bass, Henry E.
(Mississippi Univ. University, MS, United States)
Boulanger, Patrice
(Mississippi Univ. University, MS, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Publication Information
Publication: NASA. Langley Research Center, High-Speed Research: 1994 Sonic Boom Workshop: Atmospheric Propagation and Acceptability Studies
Subject Category
Acoustics
Accession Number
95N14886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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