Computation of the boundary layer and separation lines on inclined ellipsoids and of separated flows on infinite swept wings-Reference-Cited by-同舟云学术

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Computation of the boundary layer and separation lines on inclined ellipsoids and of separated flows on infinite swept wings

Published:1980-07-14 Issue: Volume: Page:
ISSN:
Container-title:13th Fluid and PlasmaDynamics Conference
language:
Short-container-title:

Author:

STOCK H.¹

Affiliation:

1. Dornier GmbH, Friedrichshafen, West Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1442

Reference35 articles.

1. T. CEBECI, K. KAUPS, J.A. RAMSEY A General Method for Calculating Three-Dimensional Compressible Laminar and Turbulent Boundary Layers on Arbitrary Wings NASA CR-2777 (1977)

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Cross-flow separation on a prolate spheroid at angles of attack;30th Aerospace Sciences Meeting and Exhibit;1992-01-06

2. On three-dimensional flow separation criteria;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24

3. Laminar separating flow over a prolate spheroid;Journal of Aircraft;1989-09

4. The position of laminar separation lines on smooth inclined bodies;AIAA Journal;1985-06

5. Transonic small-disturbance theory for dusty gases;AIAA Journal;1985-06

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