Low-speed characteristics for the wing-canard configuration of the International Vortex Flow Experiment
Author:
Affiliation:
1. Institut fur Stromungsmechanik, Braunschweig D-38106, Germany
2. Dornier Luftfahrt GmbH, Wessling D-82230, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46573
Reference21 articles.
1. Vortex trajectories and breakdown on wing-canard configurations
2. Effect of wing/canard interference on the loading of a delta wing
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