Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft-Reference-Cited by-同舟云学术

Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft

Published:2008-01 Issue:1-2 Volume:17 Page:217-243
ISSN:1779-7179
Container-title:European Journal of Computational Mechanics
language:fr
Short-container-title:European Journal of Computational Mechanics

Author:

Maute Kurt¹,Farhat Charbel²,Argrow Brian¹,Nikbay Melike³

Affiliation:

1. a Department of Aerospace Engineering Sciences , University of Colorado , Boulder , CO , 80309 , USA

2. b Department of Mechanical Engineering and Institute for Computational and Mathematical Engineering , Stanford University , Stanford , CA , 94305 , USA

3. c Faculty of Aeronautics and Astronautics , Istanbul Technical University Maslak , 34469 , Istanbul , Turkey

Publisher

River Publishers

Subject

Mechanical Engineering,Mechanics of Materials,Modelling and Simulation

Link

https://www.tandfonline.com/doi/pdf/10.3166/remn.17.217-243

Reference43 articles.

1. Efficient modeling in shape optimal design

2. Busemann, A. The Relation between Minimizing Drag and Noise at Supersonic Speeds. Proceedings of High Speed Aerodynamics. pp.133–144. Polytechnic Institute of Brooklyn.

3. Sonic Boom Theory: Its Status in Prediction and Minimization

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