Gudunov-method computation of the flow field associated with a sonic-boom focus
Author:
Affiliation:
1. Mount Auburn Research Associates, Inc.,Newton, Mass.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-240
Reference14 articles.
1. Supersonic Turns without Superbooms
2. W. D. Hayes, R. C. Haefele, and H. E. Kulsrud, "Sonic Boom Propagation i n a ;tratified Atmosphere with Computer Program, NASA CR-1299 (1969).
3. A Numerical Method for Predicting the Pressure History of a Sonic Boom Wave Incident on Arbitrarily Oriented Plane Walls
4. S. K. Godunov, A. E. Zabrodin, and 6. P. Prokopov, "A Difference Scheme for a Two-Dimensional Unsteady Problem i n Gas Dynamics and the Calculation of a Flow with a Detached Shock Wave, USSR, Computational Mathematics and Mathematical Physics 1,pp. 1187-1219 (1962).
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1. Reduction of the sonic boom level by heating the flow in front of the body;Shock Waves;2014-03-25
2. Controlling the sonic boom from a thin body by means of local heating of the incoming flow;Shock Waves;2013-07-11
3. Calculation of shock-wave parameters far from origination by combined numerical-analytical methods;Journal of Applied Mechanics and Technical Physics;2011-03
4. Review of sonic boom theory;12th Aeroacoustic Conference;1989-04-10
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