Numerical investigation of the flow structure around a rapidly pitching airfoil-Reference-Cited by-同舟云学术

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Numerical investigation of the flow structure around a rapidly pitching airfoil

Published:1987-06-08 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

VISBAL MIGUEL¹,SHANG JOSEPH¹

Affiliation:

1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1424

Reference29 articles.

1. seen that for the cases when X,/c = 0.5 and x./c = 0.75 the torque exerted by the fluid on the airfoil is in the direction of rotation, and consequently, the airfoilpp.285-311. extracts energy from the surrounding stream.

2. Airfoil dynamic stall performance with large-amplitude motions

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1. Wake-structure interaction of flow over a freely rotating hydrofoil in the wake of a cylinder;Journal of Fluids and Structures;2023-05

2. Influence of the pivot location on the thrust and propulsive efficiency performance of a two-dimensional flapping elliptic airfoil in a forward flight;Physics of Fluids;2021-08

3. Unsteady viscous flow computations using a two-equation turbulence model with wall functions;14th Applied Aerodynamics Conference;1996-06-17

4. Navier-Stokes methods to predict circulation control airfoil performance;Journal of Aircraft;1992-03

5. Computation of vortex-dominated flow for a delta wing undergoing pitching oscillation;AIAA Journal;1990-09

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