An algorithm for unsteady transonic flow about tapered wings-Reference-Cited by-同舟云学术

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An algorithm for unsteady transonic flow about tapered wings

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

BORLAND C.¹,SOTOMAYER W.²

Affiliation:

1. Boeing Military Airplane Co., Seattle, WA

2. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1567

Reference16 articles.

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. Calculation of steady and unsteady pressures on wings at supersonic speeds with a transonic small-disturbance code;Journal of Aircraft;1991-03

2. Unsteady transonic flow calculations for realistic aircraft configurations;Journal of Aircraft;1989-01

3. Computational Methods for Unsteady Transonic Flows;Unsteady Transonic Aerodynamics;1989-01-01

4. Efficient algorithm for solution of the unsteady transonic small-disturbance equation;Journal of Aircraft;1988-07

5. Calculation of transonic steady and oscillatory pressures on a low aspect ratio model;Journal of Aircraft;1987-06

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