Progress Towards Multidisciplinary Design Optimization of Truss Braced Wing Aircraft with Flutter Constraints-Reference-Cited by-同舟云学术

Progress Towards Multidisciplinary Design Optimization of Truss Braced Wing Aircraft with Flutter Constraints

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference
language:
Short-container-title:

Author:

Bhatia Manav¹,Gur Ohad¹,Kapania Rakesh¹,Mason William¹,Schetz Joseph¹,Haftka Raphael²

Affiliation:

1. Virginia Polytechnic Institute and State University

2. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9077

Reference26 articles.

1. Systematic review of the impact of emissions from aviation on current and future climate

2. Emissionless Aircraft Study

3. Laminar Flow Control - Back to the Future?

4. 4Pfenninger, W. “Laminar Flow Control Laminarization”, AGARD Report 654, “Special Course on Concepts for Drag Reduction” , 1977, Summarized from the report “Some thoughts on the design of large global rangeLFCtransport airplanes”, Jan., 1976.

5. Multidisciplinary Design Optimization of a transonic strut-braced wing aircraft

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