Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104

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

Published:2018-05 Issue:3 Volume:55 Page:1050-1061
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

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

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034415

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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