Effective flow control for rotorcraft applications at flight Mach numbers
Author:
Affiliation:
1. Illinois Inst. of Technology, Chicago, IL
2. Tel Aviv Univ., Israel; Arizona, Univ., Tucson
3. Boeing Co., Mesa, AZ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2974
Reference42 articles.
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4. Grid generation for general 2-D regions using hyperbolic equations
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