Lift Distributions on Low-Aspect-Ratio Wings at Low Reynolds Numbers for Micro-Air Vehicle Applications-Reference-Cited by-同舟云学术

Lift Distributions on Low-Aspect-Ratio Wings at Low Reynolds Numbers for Micro-Air Vehicle Applications

Author:

Sathaye Sagar¹,Yuan Jiankun¹,Olinger David¹

Affiliation:

1. Worcester Polytechnic Institute

Publisher

American Institute of Aeronautics and Astronautics

Link

Reference26 articles.

2. 3Zimmerman,C.H."CharacteristicsofClarkYairfoilsofsmallaspectratios,"NACATR431,1932.

3. 4Winter,H."Flowphenomenaonplatesandairfoilsofshortspan,"NACATM798,1936.

4. Hoerner,S.F.,Fluid-DynamicDrag,HoernerFluidDynamics,Bricktown,NJ,1965.

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