Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference Schemes
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50450
Reference18 articles.
1. Kutler, P. "Application of Selected Finite Difference Techniques to the Solution of Conical Flow Problems," Ph.D. thesis,1969, Iowa State Univ., Dept. of Aerospace Engineering, Ames, Iowa.
2. Shock-Capturing, Finite-Difference Approach to Supersonic Flows
3. Second- and Third-Order Noncentered Difference Schemes for Nonlinear Hyperbolic Equations
4. Three-dimensional flow calculation by the method of characteristics.
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