Computation of hypersonic viscous flow over a body with mass transfer and/or spin
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28364
Reference12 articles.
1. Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt Bodies
2. Heat- and mass-transfer effects on three-dimensional hypersonic viscous shock-layer flows
3. NUMERICAL SOLUTIONS TO THE VISCOUS SHOCK-LAYER BLUNT BODY PROBLEM WITH INERT GAS INJECTION.
4. Calculation of the Flow on a Cone at High Angle of Attack
5. 5Waskiewicz, J.D. and Lewis, C.H. "Hypersonic Viscous Flows over Sphere-Cones at High Angles of Attack," AIAA Paper 78-64, Jan.1978.
Cited by 4 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. Investigation of swirling flow of a viscous gas near the stagnation line of a blunt body;Journal of Applied Mechanics and Technical Physics;1989
2. Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing;Fluid Dynamics;1986
3. Comparative analysis of numerical schemes for hypersonic re-entry flows;Journal of Spacecraft and Rockets;1985-09
4. AN IMPLICIT PARABOLIZED NAVIER-STOKES SCHEME FOR HIGH ALTITUDE REENTRY FLOW;23rd Aerospace Sciences Meeting;1985-01-14
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