A fast algorithm for the calculation of transonic flow over wing/body combinations-Reference-Cited by-同舟云学术

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A fast algorithm for the calculation of transonic flow over wing/body combinations

Published:1981-06-22 Issue: Volume: Page:
ISSN:
Container-title:5th Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

BAKER T.¹,FORSEY C.¹

Affiliation:

1. Aircraft Research Association, Ltd., Bedford, England

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1015

Reference6 articles.

1. Potential Flow', VKI Lecture Series 1981-5 on Computational Fluid Dynamics,von Karman Institute for Fluid Dynamics, Rhode-St-GenPse,

2. Belgium, March 1981. 13. Ballhaus W F, Steger J L, 'Implicit

3. Assessment', AGARD-AR-138, 1979. 15. Rizzi A, Eriksson L E, 'Transfinite Mesh

4. Configurations', AIM Paper 81-0999, 1981. 16. Jameson A, 'Acceleration of Transonic

Cited by 4 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. Approximate factorization scheme for transonic potential flow computations;Sadhana;1992-06

2. Computation of transonic potential flow past wing-body configurations;Acta Mechanica;1990-09

3. Numerical solution of transonic wing flowfields;AIAA Journal;1983-06

4. Damped Euler-equation method to compute transonic flow around wing-body combinations;AIAA Journal;1982-10

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