Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control-Reference-Cited by-同舟云学术

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Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control

Published:2018-05 Issue:3 Volume:55 Page:1090-1102
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hitzel Stephan Maria¹,Osterhuber Robert¹

Affiliation:

1. Airbus Defence and Space, 85077 Manching, Germany

Funder

Stephan Maria Hitzel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034473

Reference34 articles.

1. LanchesterF. W., Aircraft in Warfare, The Dawn of the Fourth Arm, Constable & Co, London, 1916, pp. 74–94.

2. HummelD. “On the Vortex Formation over a Slender Wing at Large Angles of Incidence,” AGARD CP-247, Neuilly sur Seine, France, Oct. 1978.

3. BrennenstuhlU.HummelD. “Vortex Formation over Double-Delta Wings,” International Council of Aerospace Sciences Paper ICAS-82-6.6.3, 1982.

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