Practical design optimization of wing/body configurations using the Euler equations-Reference-Cited by-同舟云学术

Practical design optimization of wing/body configurations using the Euler equations

Published:1992-06-22 Issue: Volume: Page:
ISSN:
Container-title:10th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

REUTHER J.¹,CLIFF S.¹,HICKS R.¹,VAN DAM C.²

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

2. California, University, Davis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2633

Reference14 articles.

1. Middleton, W. D. and Lundry, J. L. "A System for Aerodynamic Design and Analysis of Supersonic Aircraft, Part 1 - General Description and Theoretical Description,"NASA CR-3351, Dec. 1980.

2. Masuda, K. and Yoshida, K. "Improvingthe Lift and Drag Characteristics of SST,"AIAA paper 91-3105, Sept. 1991.

3. Bushnell, D. "Supersonic Aircraft Drag Reduction,"AIAApaper 90-1596,June 1990.

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