The flow about a slender cone at hypersonic speeds in the weak interaction regime-Reference-Cited by-同舟云学术

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The flow about a slender cone at hypersonic speeds in the weak interaction regime

Published:1971-06-21 Issue: Volume: Page:
ISSN:
Container-title:4th Fluid and Plasma Dynamics Conference
language:
Short-container-title:

Author:

VAS I.¹,ZAKKAY V.²

Affiliation:

1. PRINCETON U., PRINCETON, N.J.

2. NEW YORK U., NEW YORK, N.Y.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1971-625

Reference29 articles.

1. Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies

2. Garvine, R. )I. "On Upstream Influcncc in Viscous Interaction Problems", H67SD111, Spacc Scicrices Iaboratory, General Llcctric, Dcc.1967.

3. Levine, J. N. "Finite Diffcrcnce Solution of the Laminar Boundary Iayer Equationr, Including Second-Order Effects", AIAA laper No. 68-739, A I M Fluid and Plasm Dynamics Confcrcncc, Las Angeles, Calif./Junc 24-26, Ig68.

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1. A Survey of the Utilitarian Aspects of Advanced Flowfield Diagnostic Techniques;AIAA Journal;1979-12

2. A survey of the utilitarian aspects of advanced flow-field diagnostic techniques;10th Aerodynamic Testing Conference;1978-04-19

3. Heat Flux Probe as a Flowfield Diagnostic;AIAA Journal;1973-11

4. Flowfield Measurements Using a Total Temperature Probe at Hypersonic Speeds;AIAA Journal;1972-03

5. The flow about a slender cone at hypersonic speeds in the weak interaction regime;4th Fluid and Plasma Dynamics Conference;1971-06-21

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