Reply to 0.R. Burggraf
Author:
Affiliation:
1. Avco Corporation, Wilmington, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55263
Reference11 articles.
1. Transverse Curvature Effects in Axisymmetric Hypersonic Boundary Layers
2. Displacement thickness for boundary layers with surface mass transfer.
3. JUNE1966 TECHNICAL COMMENTS
4. Transverse Curvature Effects in Axisymmetric Hypersonic Boundary Layers
Cited by 5 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. Binary boundary layers on sharp cones in low-density supersonic and hypersonic flow;6th Aerospace Sciences Meeting;1968-01-22
2. Theoretical studies on the effects of blowing and suction in laminarseparated regions.;Journal of Spacecraft and Rockets;1967-10
3. A comment on hypersonic viscous interaction theory.;AIAA Journal;1967-07
4. Comments on "Displacement Thickness for Boundary Layers with Surface Mass Transfer";AIAA Journal;1967-04
5. Theoretical studies on the effects of blowing and suction in laminarseparated regions;5th Aerospace Sciences Meeting;1967-01-23
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