Hybrid feedback design for subsonic and transonic airfoils and wings-Reference-Cited by-同舟云学术

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Hybrid feedback design for subsonic and transonic airfoils and wings

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Zhang Mengmeng¹,Wang Cong¹,Rizzi Arthur W.¹,Nangia R K.²

Affiliation:

1. Royal Institute of Technology (KTH)

2. Bristol University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0414

Reference19 articles.

1. A hybrid algorithm for transonic airfoil and wing design

2. 3Takanashi, S., An iterative procedure for three-dimensional transonic wing design by the integral equation method, AIAA paper 84-2155.

3. 4Drela,M., Newton solution of coupled viscous/inviscid multielement airfoil flows. AIAA Paper 90-1470.

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