General Approach to Lifting-Line Theory, Applied to Wings with Sweep-Reference-Cited by-同舟云学术

General Approach to Lifting-Line Theory, Applied to Wings with Sweep

Published:2021-03 Issue:2 Volume:58 Page:334-346
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Reid Jackson T.¹,Hunsaker Douglas F.¹

Affiliation:

1. Utah State University, Logan, Utah 84321

Funder

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035994

Reference36 articles.

1. PrandtlL., Tragflügel Theorie, Nachricten von der Gesellschaft der Wissenschaften zu Göttingen, Geschäeftliche Mitteilungen, Klasse, 1918, pp. 451–477.

2. PrandtlL. “Appplications of Modern Hydrodynamics to Aeronautics,” NACA TR-116, June 1921.

3. AndersonJ. D., Fundamentals of Aerodynamics, 5th ed. McGraw–Hill, New York, 2011, pp. 1–486, Chaps. 1–5.

4. PhillipsW. F., Mechanics of Flight, 2nd ed. Wiley, Hoboken, NJ, 2010, pp. 1–134, Chap. 1.

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