Defining the Aerothermodynamic Methodology-Reference-Cited by-同舟云学术

Defining the Aerothermodynamic Methodology

Published:1989 Issue: Volume: Page:125-204
ISSN:
Container-title:Hypersonics
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Author:

Neumann Richard D.

Publisher

Birkhäuser Boston

Link

http://link.springer.com/content/pdf/10.1007/978-1-4684-9187-6_4.pdf

Reference120 articles.

1. Adams, J.C. “Real Gas Scale Effects on Hypersonic Laminar Boundary Layer Parameters Including Effects of Entropy Layer Swallowing”, AEDC TR 75-2, 1975

2. Adams, J.C. and Griffith, B.J., “Hypersonic Viscous Static Stability of a Sharp Five Degree Coneat Incidence” AIAA Journal, Volume 14, No 8, pp 1062–1068, 1976

3. Anders, J.B. and C.L.W. Edwards “A Real-Gas Study of Low Density Wedge-Induced Laminar Separation of a Highly Separation on a Highly Cooled Blunt Flat Plate at M=12”, NASA TN D-4320, 1968

4. Arrington, J.P. and Henderson, A., “Effect of Reynolds Number on the Stability of a Blunt-Nosed Flared Cylinder from Mach 17.6 to 22.2 in Helium”, NASA TM X 1166, 1965

5. Baradell, D.L. and McLellan, C.H., “Lateral range and Hypersonic Lift to Drag Requirements for Efficient Ferry Service From a Near Earth Manned Space Station”, Proceedings of the AIAA 2nd Manned Space Flight Symposium, pp. 159 ff, 1963

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