Newtonian Flow Theory for Slender Bodies
Author:
Affiliation:
1. The RAND Corporation and California Institute of Technology,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3875
Reference21 articles.
1. Three-Dimensional Laminar Boundary-Layer Flow
2. Staff of the Computing Section, Center of Analysis (under direction of Kopal, Z.), Tables of Supersonic Flow Around Yawing Cones, M.I.T. Technical Report No. 3, 1947.
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