Supersonic transport wing minimum weight design integrating aerodynamics and structures-Reference-Cited by-同舟云学术

Supersonic transport wing minimum weight design integrating aerodynamics and structures

Published:1994-03 Issue:2 Volume:31 Page:330-338
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Barthelemy J.-F. M.,Coen P. G.,Wrenn G. A.,Dovi A. R.,Hall L. E.¹

Affiliation:

1. Unisys Corporation, Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46491

Reference15 articles.

1. 'Barthelemy, J.F. M., Coen, P. G., Wrenn, G. A., Riley, M. F., Dovi, A. R., and Hall, L. E. "Application of Multidisciplinary Optimization Methods to the Design of a Supersonic Transport," NASA TM-104073, March'1991.

2. Sensitivity of complex, internally coupled systems

3. Preliminary results from the High Speed Airframe Integration Research project

4. Equivalent plate analysis of aircraft wing box structures with general planform geometry

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