Hypersonic Laminar Viscous Flow Past Spinning Cones at Angle of Attack
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51098
Reference21 articles.
1. Magnus Forces on Spinning Supersonic Cones -Part I: The Boundary Layer
2. Viscous Flow over Spinning Cones at Angle of Attack
3. Calculation of the flow on a cone at high angle of attack
Cited by 3 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. An assessment of numerical solutions of the compressible Navier-Stokes equations;Journal of Aircraft;1985-05
2. An assessment of numerical solutions of the compressible Navier-Stokes equations;17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1984-06-25
3. Numerical simulation of steady supersonic flow over spinning bodies of revolution;AIAA Journal;1982-12
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