Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104–105)

Author:

Winslow Justin1,Otsuka Hikaru1,Govindarajan Bharath1,Chopra Inderjit1

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Funder

US Army/US Navy/NASA Vertical Lift Research Center of Excellence

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference21 articles.

1. Hover Performance of a Small-Scale Helicopter Rotor for Flying on Mars

2. MuellerT. J. “Aerodynamic Measurements at Low Reynolds Numbers for Fixed Wing Micro-Air Vehicles,” RTO AVT/VKI Special Course on Development and Operation of UAVs for Military and Civil Applications, Von-Karman Inst., Brussels, Sept. 1999, http://www.dtic.mil/docs/citations/ADP010760.

3. AERODYNAMICS OF SMALL VEHICLES

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