Numerical computation of multishocked, three-dimensional supersonic flow fields with real gas effects
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-702
Reference19 articles.
1. Kutler, P., Lomax, 8. and Warming, R. F. "Computation of space ,Shuttle Flow Fields Using Noncentered Finite-Difference Schemes," AIAA Paper 72-193, 19V2.
2. The Supersonic Flow Past an Elliptic Cone
3. v AIAA Paper 12-27, 1912.
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1. Simulation of viscous hypersonic flows past hyperboloid configurations with flare;29th Aerospace Sciences Meeting;1991-01-07
2. Conservation form of the Navier-Stokes equations in general nonsteady coordinates;AIAA Journal;1981-02
3. Aerodynamic prediction methodology for maneuvering reentry vehicles;6th Atmospheric Flight Mechanics Conference;1980-08-11
4. Geometric Conservation Law and Its Application to Flow Computations on Moving Grids;AIAA Journal;1979-10
5. The Geometric Conservation Law - A link between finite-difference and finite-volume methods of flow computation on moving grids;11th Fluid and PlasmaDynamics Conference;1978-07-10
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