Boundary-Layer Separation on Slender Cones at Angle of Attack
Author:
Affiliation:
1. Aerospace Research Laboratories, Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50169
Reference22 articles.
1. A Study of General Three-Dimensional Boundary-Layer Problems by an Exact Numerical Method
2. Inviscid flowfield about a pointed cone at an angle of attack.
3. A method of solving the three-dimensional laminar boundary-layer equations with application to a lifting re-entry body.
4. Laminar boundary layer on a cone at incidence in supersonic flow
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