Boundary-Layer Separation on Slender Cones at Angle of Attack
- 1 May 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (5), 642-648
- https://doi.org/10.2514/3.50169
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- A Study of General Three-Dimensional Boundary-Layer Problems by an Exact Numerical MethodAIAA Journal, 1971
- An Experimental Investigation of the Flowfield around a Yawed ConeAIAA Journal, 1971
- Laminar boundary layer on a cone at incidence in supersonic flowAIAA Journal, 1971
- Separation patterns of boundary layer over an inclined body of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- A method of solving the three-dimensional laminar boundary-layer equations with application to a lifting re-entry body.AIAA Journal, 1968
- Inviscid flowfield about a pointed cone at an angle of attack.AIAA Journal, 1967