Contours for stagnation-point mass injection in hypersonic flow
- 1 January 1964
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (1) , 178-179
- https://doi.org/10.2514/3.2267
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An experimental investigation of a two-layer inviscid shock cap due to blunt-body nose injectionJournal of Fluid Mechanics, 1963
- The Supersonic Blunt-Body Problem - Review and ExtensionJournal of the Aerospace Sciences, 1958
- Stagnation Point of a Blunt Body in Hypersonic FlowJournal of the Aeronautical Sciences, 1957