Dependence of optimal structural weight on aerodynamic shape for a High Speed Civil Transport-Reference-Cited by-同舟云学术

Dependence of optimal structural weight on aerodynamic shape for a High Speed Civil Transport

Published:1996-08-22 Issue: Volume: Page:
ISSN:
Container-title:6th Symposium on Multidisciplinary Analysis and Optimization
language:
Short-container-title:

Author:

Balabanov V.¹,Kaufman M.¹,Knill D.¹,Haim D.¹,Golovidov O.¹,Giunta A.¹,Haftka Raphael²,Grossman B.¹,Mason W.¹,Watson L.¹

Affiliation:

1. Virginia Polytechnic Inst. and State Univ., Blacksburg

2. Florida, Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-4046

Reference23 articles.

1. Aerodynamic optimization of an HSCT configuration using variable-complexity modeling

2. Variable-complexity aerodynamic optimization of a high-speed civil transport wing

3. Huang, X., Haftka, R. T., Grossman,B., and Mason, W. "Comparison of Statistical-based Weight Equations with Structural Optimization for Supersonic Transport Wings", AIAA 94-4379,1994.

4. Vanderplaats, Miuraand Associates, Inc., GENESIS User Manual,Version 1.3,Dec. 1993, 5960Mandarin Avenue, Suite F, Goleta, CA 93117

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