Optimization of an advanced design three-element airfoil at high Reynolds numbers /

Bibliographic Details

Main Authors:	Lin, J.-C. (Jiun-Chuan) (Author), Dominik, C. J. (Author)
Corporate Author:	American Institute of Aeronautics and Astronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
Series:	NASA technical memorandum ; 112019.
Subjects:	Airfoils. Computational fluid dynamics. High Reynolds number. Leading edges. Prediction analysis techniques.
Online Access:	https://purl.fdlp.gov/GPO/gpo77769