Experimental study on the aerodynamic effects of a forward-sweep angle
Author:
Affiliation:
1. University of Pisa, Pisa, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. A Foward-Swept-Wing Fighter Configuration Designed by a Transonic Computational Method
2. 5Kucheman, D. "The Aerodynamic Design of Aircraft," Pergamon, London, 1978, pp.103-220.
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