journal article Sep 01, 1997

Enthalpy Effects on Hypervelocity Boundary-Layer Transition: Ground Test and Flight Data

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References
18
[2]
Germain P. (1993)
[5]
Demetriades A. (1977)
[6]
Hornung H. G. (1994)
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12Germain, P. “The Boundary Layer on a Sharp Cone in High-Enthalpy Flow,” Ph.D. Thesis, Graduate Aeronautical Labs., California Inst. of Technology, Pasadena,CA, June 1994. 10.1007/978-3-642-78829-1_9
[13]
Schultz D. L. (1973)
[14]
14Sanderson, S. R. “Shock Wave Interaction in Hypervelocity Flow,” Ph.D. Thesis, Graduate Aeronautical Labs., California Inst. of Technology, Pasadena,CA, May 1995.
[15]
White F. M. (1991)
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[17]
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[18]
Clarke J. F. London (1964)
Metrics
53
Citations
18
References
Details
Published
Sep 01, 1997
Vol/Issue
34(5)
Pages
614-619
Cite This Article
Philippe H. Adam, Hans G. Hornung (1997). Enthalpy Effects on Hypervelocity Boundary-Layer Transition: Ground Test and Flight Data. Journal of Spacecraft and Rockets, 34(5), 614-619. https://doi.org/10.2514/2.3278
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