Wall cooling effects on hypersonic boundary layer transition, M(1) =7.5

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Wall cooling effects on hypersonic boundary layer transition, M(1) =7.5 - 15

Published:1986-05-12 Issue: Volume: Page:
ISSN:
Container-title:4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference
language:
Short-container-title:

Author:

NAGAMATSU H.¹,SHEER, JR. R.²,WISLER D.³

Affiliation:

1. Rensselaer Polytechnic Institute, Troy, NY

2. GE Research and Development Center, Schenectady, NY

3. GE Fluid Mechanics Laboratory, Evendale, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1088

Reference47 articles.

1. Transition of Hypersonic Boundary Layer

2. Hypersonic laminar boundary-layer transition on 8-foot-long, 10 deg cone, M sub 1 equals 9.1-16.

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