Inviscid Flowfield Calculations for Re-entry Vehicles with Control Surfaces
Author:
Affiliation:
1. Naval Surface Weapons Center/ White Oak Laboratory, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference20 articles.
1. 'Thomas, P. D., Vinokur, M., Bastianon, R., and Conti, R. J. "Numerical Solution for Three-Dimensional Inviscid Supersonic Flow/M/A/l Journal, Vol.10, July 1972, pp.887-894.
2. A complete numerical technique for the calculation of three-dimensional inviscid supersonic flows
3. 3Moretti, G. and Pandolfi, M. "Analysis of the Inviscid Flow About a Yawed Cone, Preliminary Studies," Polytechnic Inst. of Brooklyn, Dept. of Aero. Eng. and Applied Mechanics Rept. No. 72-18,1972.
4. Computation of Three Dimentional Flows about aircraft configurations
5. Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects
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