Inviscid analysis of dual-throat nozzle flows
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Split Coefficient Matrix method for hyperbolic systems of gasdynamic equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional GeometriesAIAA Journal, 1978
- Elements of GasdynamicsPhysics Today, 1957