Calculation of the laminar viscous shock layer on a blunt biconic body at incidence to supersonic and hypersonic flow
Author:
Affiliation:
1. ARO, Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-88
Reference16 articles.
1. sonic Flow over Blunt-Nascd and Flared Bodies." NASA TN 0-2970, August 1965. o-2deg grams for Two-Dimensional and Axisymmetric Super
2. 5Davis, R. T. "The Hypersonic Fully Viscous Shock-Layer Problem." Report SC-RR-68-840,Sandia Corporation,Albuquerque, New Mexico,1968. See also AIM Journal, Vol.8,No. 5, May 1970, pp.843-851.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Viscous flow over arbitrary geometries at high angle of attack;18th Aerospace Sciences Meeting;1980-01-14
2. Computation of supersonic viscous flows over ogive-cylinders at angle of attack;17th Aerospace Sciences Meeting;1979-01-15
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