Reply to T.K. Fannelop
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55262
Reference11 articles.
1. EFFECTIVE DISPLACEMENT THICKNESS FOR BOUNDARY LAYERS WITH SURFACE MASS TRANSFER
2. BLOWING EFFECTS ON PRESSURE INTERACTION ASSOCIATED WITH CONES
3. Transverse Curvature Effects in Axisymmetric Hypersonic Boundary Layers
4. SECOND-ORDER COMPRESSIBLE BOUNDARY LAYER THEORY WITH APPLICATION TO BLUNT BODIES IN HYPERSONIC FLOW
5. The laminar compressible boundary-layer in the stagnation-point region of an axisymmetric blunt body including the second-order effect of vorticity interaction
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. COMMENT ON "FINITE ELEMENTS FOR AXISYMMETRIC SOLIDS UNDER ARBITRARY LOADINGS WITH NODES OF ORIGIN';AIAA Journal;1973-09
2. Reply by Author to G.R. Inger;AIAA Journal;1973-09
3. Comment on "Skin Friction on Porous Surfaces Calculated by a Simple Integral Method";AIAA Journal;1973-09
4. A comment on hypersonic viscous interaction theory.;AIAA Journal;1967-07
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