Ideal Tail Load for Minimum Aircraft Drag-Reference-Cited by-同舟云学术

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Ideal Tail Load for Minimum Aircraft Drag

Published:1978-03 Issue:3 Volume:15 Page:190-192
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Laitone E. V.¹

Affiliation:

1. University of California, Berkeley, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference5 articles.

1. Barman, Th. von and Burgers, J. M., Durand's Aerodynamic Theory, Vol.2, Div. E,J. Springer, Berlin,1934, pp.218-220and 326-329.

2. 2Kerber, L. V., Durand's Aerodynamic Theory, Vol.5, Div. O,J. Springer, Berlin,1934, pp.333-337.

3. Trimmed drag considerations

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1. Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration;Journal of Aircraft;2016-01

2. The aerodynamics of micro air vehicles: technical challenges and scientific issues;International Journal of Engineering Systems Modelling and Simulation;2014

3. Animal Flight Dynamics I. Stability in Gliding Flight;Journal of Theoretical Biology;2001-10

4. Aerodynamic, dynamic and conceptual design of a fire-fighting aircraft;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2001-03-01

5. Why do Birds have Tails? The Tail as a Drag Reducing Flap, and Trim Control;Journal of Theoretical Biology;1996-12

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