Analytical and computational study of unsteady shock motion on hypersonic forebodies
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46059
Reference14 articles.
1. Liquid-fueled supersonic combustion ramjets - A research perspective
2. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
3. Bow shock matching with viscous effects on hypersonic forebodies
4. 5Ng, W.F. "Time Resolved Measurements in a Transonic Compressor Stage," Ph.D. Dissertation,Dept. of Mechanical Engineering, Massachusetts Inst. of Technology, Cambridge, MA,1983.
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1. Analysis of Highly Unsteady and Quasi-steady Shocks in Hypersonic Inlets Based on the Principle of Minimum Entropy Production;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24
2. Time-Averaged Entropy and Total Pressure Ratios Across Unsteady Inlet Shock Waves;Journal of Propulsion and Power;2005-11
3. Designing hypersonic inlets for bow shock location control;Journal of Propulsion and Power;1993-03
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