A shock-expansion method for determining surface properties on irregular geometries

Author:

Starkey R.1,Lewis M.

Affiliation:

1. Maryland, Univ., College Park

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Critical Design Issues for Airbreathing Hypersonic Waverider Missiles

2. A. J. Eggers, J., Syvertson, C. A., and Kraus, S. "A Study of Inviscid Flow About Airfoils at High Supersonic Speeds," NAGA Technical Report 1123, 1953.

3. The Generalized Shock-Expansion Method and Its Application to Bodies Traveling at High Supersonic Air Speeds

4. A Critique of Shock-Expansion Theory

5. A. J. Eggers, J., and Savin, R. C. "A Unified Two-Dimensional Approach to the Calculation of Three-Dimensional Hypersonic Flows, With Application to Bodies of Revolution," NACA Technical Report 1249, 1953.

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1. Six-Degree-of-Freedom Simulation of Hypersonic Vehicles;AIAA Atmospheric Flight Mechanics Conference;2009-06-14

2. Effects of Hypersonic Cruise Trajectory Optimization Coupled with Airbreathing Vehicle Design;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

3. Coupled Waverider/Trajectory Optimization for Hypersonic Cruise;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

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