Integrated Multidisciplinary Topology Optimization Approach to Adaptive Wing Design-Reference-Cited by-同舟云学术

Integrated Multidisciplinary Topology Optimization Approach to Adaptive Wing Design

Published:2006-01 Issue:1 Volume:43 Page:253-263
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Maute K.¹,Reich G. W.²

Affiliation:

1. University of Colorado at Boulder, Boulder, Colorado 80309-0429

2. U.S. Air Force Research Laboratory, Dayton, Ohio 45433-7531

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.12802

Reference51 articles.

1. 1Hall, J. "Executive Summary AFTI/F-111 Mission Adaptive Wing," Tech. Rep. WRDC-TR-89-2083, Wright Research Development Center, Wright-Patterson AirForce Base,1998.

2. Review of State of Art of Smart Structures and Integrated Systems

3. High-pressure magnetostrictive pump development: a comparison of prototype and modeled performance

4. Large-Area Aerodynamic Control for High-Altitude Long- Endurance Sensor Platforms

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