Calculation of the Flow on a Cone at High Angle of Attack-Reference-Cited by-同舟云学术

Calculation of the Flow on a Cone at High Angle of Attack

Published:1974-07 Issue:7 Volume:12 Page:965-974
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

LUBARD STEPHEN C.¹,HELLIWELL WILLIAM S.²

Affiliation:

1. R&D Associates, Santa Monica, Calif.

2. The Aerospace Corporation, El Segundo, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.49388

Reference25 articles.

1. Tracy, R. R. "Hypersonic Flow Over a Yawed Circular Cone," Ph.D. thesis,Aug. 1963, Aeronautical Labs., Firestone Flight Sciences Lab.Graduate California Institute of Technology, Pasadena, Calif.

2. Boundary-Layer Separation on Slender Cones at Angle of Attack

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