Boundary layer on a hypersonic sharp cone at small angle of attack
- 1 February 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (2) , 277-284
- https://doi.org/10.2514/3.6163
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Finite difference methods of solution of the boundary-layer equationsAIAA Journal, 1970
- Laminar boundary layer on a cone at incidence in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- A method of solving the three-dimensional laminar boundary-layer equations with application to a lifting reentry bodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- The vortical layer on an inclined coneJournal of Fluid Mechanics, 1964