Theoretical and experimental study of supersonic steady flow around inclined bodies of revolution
- 1 March 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (3) , 511-518
- https://doi.org/10.2514/3.5698
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- Three-dimensional flow calculation by the method of characteristics.AIAA Journal, 1967
- The Method of Characteristics for Three-Dimensional Real -Gas Flows Including the Digital Computer Program Details and Operating Procedures for Frozen FlowsPublished by Defense Technical Information Center (DTIC) ,1967
- Numerical calculations of multidimensional and unsteady flows by the method of characteristicsJournal of Computational Physics, 1967
- Calculation of hypersonic flow over bodies of revolution at small angles of attackAIAA Journal, 1965