Joint Computational-Experimental Investigation of Harmonically Pitching Airfoil Aerodynamics in Uniform-Shear Approach Flow
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058232
Reference32 articles.
1. Vortical patterns in the wake of an oscillating airfoil
2. Study of the vortical wake patterns of an oscillating airfoil
3. Oscillating foils of high propulsive efficiency
4. Jet Characteristics of a Plunging Airfoil
5. Simulation of Flow About Flapping Airfoils Using Finite Element Incompressible Flow Solver
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