Applications of MEMS devices to delta wing aircraft - From concept development to transonic flight test
Author:
Affiliation:
1. California, Univ., Los Angeles
2. California Inst. of Technology, Pasadena
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-124
Reference47 articles.
1. A Conceptual Study of Leading-Edge-Vortex Enhancement by Blowing
2. The control of vortical lift on delta wings by tangential leading edge blowing
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