Hypersonic boundary layer studies on a spinning sharp cone at angle of attack
- 25 January 1971
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Laminar boundary layer on a cone at incidence in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Reply by Author to E. KrauseAIAA Journal, 1969
- Comment on "Solution of a Three-Dimensional Boundary-Layer Flow with Separation"AIAA Journal, 1969
- Solution of a three-dimensional boundary-layer flow with separation.AIAA Journal, 1968
- The vortical layer on an inclined coneJournal of Fluid Mechanics, 1964
- Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic FlowJournal of the Aeronautical Sciences, 1957
- XLII. The laminar boundary layer of a rotating body of revolutionJournal of Computers in Education, 1953