Unsteady Aerodynamics Over NACA0005 Airfoil for Ultra-Low Reynolds Numbers
Author:
Affiliation:
1. Applied Research Center for Metrology, Standards and Testing, King Fahd University of Petroleum and Minerals (KFUPM), Dhahran, Saudi Arabia
2. Aerospace Engineering Department, Middle East Technical University (METU), Ankara, Turkey
Funder
King Fahd University of Petroleum and Minerals
Applied Research Centre for Metrology Standards and Testing, KFUPM
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx8/6287639/10380310/10555216.pdf?arnumber=10555216
Reference47 articles.
1. Hover Performance of a Small-Scale Helicopter Rotor for Flying on Mars
2. Aerodynamic performance of a characteristic airfoil at low-Reynolds number and transonic flow under Mars sand-containing environment
3. Design optimization of airfoils at ultra-low Reynolds numbers;Xu
4. Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104–105)
5. CFD vs. XFOIL of airfoil analysis at low reynolds numbers
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