High-fidelity Aerodynamic Shape Optimization of Unconventional Aircraft through Axial Deformation-Reference-Cited by-同舟云学术

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High-fidelity Aerodynamic Shape Optimization of Unconventional Aircraft through Axial Deformation

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

Author:

Gagnon Hugo¹,Zingg David W.¹

Affiliation:

1. University of Toronto

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0908

Reference50 articles.

1. Civil aviation and the environment – the next frontier for the aerodynamicist

2. DRAG DUE TO LIFT: Concepts for Prediction and Reduction

3. 4Munk, M. M. “The Minimum Induced Drag of Aerofoils,” Tech. Rep. 121, National Advisory Committee for Aeronautics, 1921.

4. 5Mangler, W. “The Lift Distribution of Wings with End Plates,” Tech. Rep. 856, National Advisory Committee for Aeronautics, 1938.

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