Shock Capturing Numerical Method for Calculating - Supersonic Flows
- 1 May 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (5) , 642-647
- https://doi.org/10.2514/3.49312
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971
- Exact and Approximate Solutions for the Supersonic Delta WingJournal of the Aeronautical Sciences, 1956
- On the solution of nonlinear hyperbolic differential equations by finite differencesCommunications on Pure and Applied Mathematics, 1952