Surface conditions on hyperboloids and paraboloids in hypersonic flow
Author:
Affiliation:
1. ARO, INC., VON KARMAN GAS DYNAMICS FACILITY, ARNOLD AIR FORCE STATION, TENN.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1970-182
Reference18 articles.
1. Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies
2. 3Van Dyke, M. "A Review and Extension of Second-Order Avversonic Boundarv-Laver Theory *' Rarefieh'Cas Dynamics, 3. A: Laucrmann, editor Fluid Symposium Supplement 2 , Vol.11. Academic Press, New York,1963, pp.37-75.
3. HIGHER ORDER BOUNDARY-LAYER EFFECTS ON ANALYTIC BODIES OF REVOLUTION
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1. Numerical Solution of the Hypersonic Viscous Shock-Layer Equations;Journal of Spacecraft and Rockets;2003-09
2. Hypersonic viscous shock-layer solutions over long slender bodies. II - Low Reynolds number flows;Journal of Spacecraft and Rockets;1990-03
3. Low Reynolds number flow past a blunt axisymmetric body at angle of attack;AIAA Journal;1977-08
4. Numerical solution of the hypersonic viscous shock-layer equations;AIAA Journal;1970-05
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