Aerodynamic Response of a NACA-0012 Airfoil Undergoing Non-Sinusoidal Pitching Waveforms
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
2. Military Technical College
3. Stevens Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0303
Reference32 articles.
1. Flowfield Measurements over an Airfoil During Natural Low-Frequency Oscillations near Stall
2. Vortex-shedding characteristics in the wake of an oscillating airfoil at low Reynolds number
3. PIV Measurements of a plunging Airfoil at High Angles of Attack
4. Numerical Investigations into the Nonsinusoidal Motion Effects on Aerodynamics of a Pitching Airfoil
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