Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications-Reference-Cited by-同舟云学术

Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications

Published:2018-06 Issue:6 Volume:56 Page:2389-2402
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Mallik Wrik¹,Schetz Joseph A.¹,Kapania Rakesh K.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056218

Reference41 articles.

1. PfenningerW. “Laminar Flow Control Laminarization,” Special Course on Concepts for Drag Reduction, AGARD Special Course on Concepts for Drag Reduction Rept. 654, NASA Langley Research Center, Hampton, VA, June 1977, pp. 3–1.

2. Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft

3. Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Transport Aircraft

4. Effect of Flutter on the Multidisciplinary Design Optimization of Truss-Braced-Wing Aircraft

5. Aeroelastic Applications of a Variable-Geometry Raked Wingtip

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