Cooling by Discrete and Porous Injection into a Turbulent, Supersonic Boundary Layer-Reference-Cited by-同舟云学术

Cooling by Discrete and Porous Injection into a Turbulent, Supersonic Boundary Layer

Published:1974-12 Issue:12 Volume:12 Page:1679-1686
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

CLARK K. J.¹,NARDO C. T.¹,JAFFE N. A.¹,COVINGTON M. A.²

Affiliation:

1. Acurex Corporation, Mountain View, Calif.

2. NASA Ames Research Center, Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.49578

Reference10 articles.

1. Jaffe, N. A, Clark, K. J., Nardo, C. T, and Anderson, L. W. "Nosetip Cooling Technology Program," Final Report 73-84, Air Force Contract F04701-71-C-0087, Oct. 1973, Aerotherm Div., Acurex Corp., Mountain View,Calif.

2. Turbulent Flow Studies in Two Arc-Heated Duct Facilities

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