Investigations on the vorticity sheets of a close-coupled delta-canard configuration-Reference-Cited by-同舟云学术

Investigations on the vorticity sheets of a close-coupled delta-canard configuration

Published:1989-07 Issue:7 Volume:26 Page:657-666
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Oelker Hans-Christoph¹,Hummel Dietrich¹

Affiliation:

1. Technische Universitat Braunschweig, Braunschweig, Federal Republic of Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45817

Reference40 articles.

1. 2Bates, W. R. * 'Low-Speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60° Triangular Wing and Horizontal Trail," NACA RM-L9H17, Nov. 1949.

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