Potential flow applications to the prediction of the F-18E aircraft flowfield-Reference-Cited by-同舟云学术

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Potential flow applications to the prediction of the F-18E aircraft flowfield

Published:1994-06-20 Issue: Volume: Page:
ISSN:
Container-title:12th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Cenko A.¹,Piranian A.¹

Affiliation:

1. NAWCADWAR, Warminster, PA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1842

Reference10 articles.

1. Erickson, L. L., et al. "Applications of the TranAir Full-Potential Code to Complete Configurations,"ICAS Paper ICAS86-1.3.5,1986.

2. TranAir applications to predicting transonic aircraft/store loads

3. Paulk, R.A., and Humes, R.L. "AnAerodynamic Loads and separation Trajectory Wind Tunnel Test With the AMRAAM Missile and the F-18 Aircraft at Mach Numbers 0.5 to 1.6, AEDC-TSR-83-P7, April 1983.

4. Cenko, A. "Determination of the F-18E Aircraft Flowfield Effects on Store Loads," NAWCADWAR Report 93049-60,Jan. 1993.

Cited by 1 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. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01

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