Euler-Equation-Based Drag Minimization of Unconventional Aircraft Configurations-Reference-Cited by-同舟云学术

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Euler-Equation-Based Drag Minimization of Unconventional Aircraft Configurations

Published:2016-09 Issue:5 Volume:53 Page:1361-1371
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Gagnon Hugo¹,Zingg David W.¹

Affiliation:

1. University of Toronto, Toronto, Ontario M3H 5T6, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033591

Reference61 articles.

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

2. BushnellD. M. “Frontier Aerospace Opportunities,” NASA TR-TM-2014-218519, 2014.

3. VKI Lecture Series;Kroo I.,2005

4. MunkM. M. “The Minimum Induced Drag of Aerofoils,” NACA TR-121, 1923.

5. PrandtlL. “Induced Drag of Multiplanes,” NACA TR-TN-182, 1924.

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