Reducing Wind Tunnel Data for Flowfield Study over the Wing-Canard Configuration Using Neural Network-Reference-Cited by-同舟云学术

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Reducing Wind Tunnel Data for Flowfield Study over the Wing-Canard Configuration Using Neural Network

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Abbasi Hoseini Afshin¹,Masdari Mehran¹

Affiliation:

1. Sharif University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-727

Reference19 articles.

1. 2-Behrbohm, H. "Basic low speed aerodynamics of the short-coupled canard configuration of small aspect ratio", SAABTN60,1965.

2. 3-Gloss, B.B. and Miner, D.D. "Flow visualization study of close-coupled canard-wing and strake-wing configurations",NASATMX-75663,1975.

3. Vortex trajectories and breakdown on wing-canard configurations

4. Effect of wing/canard interference on the loading of a delta wing

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