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Three-Dimensional Viscous Drag Prediction for Rotor BladesThe state-of-the-art in rotor blade drag prediction involves the use of two-dimensional airfoil tables to calculate the drag force on the blade. One of the most serious problems with the current methods is that they cannot be used for airfoils that have yet to be tested. Most of the drag prediction methods also do not take the Reynolds number or the rotational effects of the blade into account, raising doubts about the accuracy of the results. These problems are addressed with the development of an analytical method which includes the shape of airfoil, the effects of Reynolds number, and the rotational motion of the blade.
Document ID
19910001552
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Ching S Chen
(National Research Council Washington, DC., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: NASA Computational Fluid Dynamics Conference. Volume 1: Sessions 1-6
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Aerodynamics
Report/Patent Number
NASA-CP-10038-VOL-1
Meeting Information
Meeting: NASA Computational Fluid Dynamics Conference
Location: Moffett Field, CA
Country: US
Start Date: March 7, 1989
End Date: March 9, 1989
Sponsors: National Aeronautics and Space Administration
Accession Number
91N10865
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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