Axisymmetric Inlet Flow at Low Supersonic Mach Numbers
- 1 January 1976
- book chapter
- Published by Springer Nature
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Calculation of transonic flow around axisymmetric inletsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Analysis of Embedded Shock Waves Calculated by Relaxation MethodsAIAA Journal, 1974
- Transonic flow analysis using a streamline coordinate transformationprocedurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973