Mach Cutoff Analysis and Results from NASA's Farfield Investigation of No-boom Thresholds-Reference-Cited by-同舟云学术

Mach Cutoff Analysis and Results from NASA's Farfield Investigation of No-boom Thresholds

Published:2016-05-27 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA/CEAS Aeroacoustics Conference
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Author:

Cliatt Larry J.¹,Hill Michael A.¹,Haering Edward¹

Affiliation:

1. NASA Armstrong Flight Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3011

Reference20 articles.

1. 1Dowling,A.P.,andFfowcsWilliams,J.E.,SoundandSourcesofSound,EllisHorwoodLimited,Chichester,England,1989, p. 91.

2. 2Maglieri, D. J., Bobbitt, P. J., Plotkin, K. J., Shepherd, K. P., Coen, P. G., and Richwine, D. M. "Sonic Boom: Six Decades ofResearch,"NASA/SP-2014-622, 2014.

3. Sonic boom in the shadow zone: A geometrical theory of diffraction

4. 4Haglund, G. T., and Kane, E. J. "Flight Test Measurement and Analysis of Sonic Boom Phenomena Near the Shock Wave Extremity,"NASACR-2167,1973.

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