A Computational Study on the Dynamic Stall of a Flapping Airfoil
dc.contributor.author | Tuncer, Ismail | |
dc.contributor.author | Walz, Ralf | |
dc.contributor.author | Platzer, Max F. | |
dc.date | 1998 | |
dc.date.accessioned | 2016-10-14T15:10:26Z | |
dc.date.available | 2016-10-14T15:10:26Z | |
dc.date.issued | 1998 | |
dc.identifier.citation | Tuncer, Ismail H., Ralf Walz, and Max F. Platzer. "A computational study on the dynamic stall of a flapping airfoil." AIAA paper 2519 (1998): 1998. | en_US |
dc.identifier.uri | https://hdl.handle.net/10945/50285 | |
dc.description | The article of record as published may be found at http://dx.doi.org/10.2514/6.1998-2519 | en_US |
dc.description.abstract | The dynamic stall boundaries of a NACA 0012 airfoil oscillating in either the pure plunge mode or in the combined pitch and plunge mode is computed using a thin-layer Navier-Stokes solver. Unsteady flowfields are computed at the free-stream Mach number of 0.3, the Reynolds number of 1 • 106, and the Baldwin-Lomax turbulence model is employed. It is found that the pure plunge oscillation leads to dynamic stall as soon as the non-dimensional plunge velocity exceeds the approximate value of 0.35. In addition, the power extraction capability of the airfoil operating in the wingmill mode is studied by computing the dynamic stall boundary for a combined pitch and plunge motion at the reduced frequency values of 0.1, 0.25 and 0.5. | en_US |
dc.description.sponsorship | Naval Research Laboratory | en_US |
dc.format.extent | 7 p. | en_US |
dc.publisher | American Institute of Aeronautics and Astronautics, Inc. | en_US |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | en_US |
dc.title | A Computational Study on the Dynamic Stall of a Flapping Airfoil | en_US |
dc.type | Article | en_US |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | en_US |
dc.description.funder | Naval Research Laboratory | en_US |