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

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Bibliographic Details
Author / Creator:	Lin, J.-C. (Jiun-Chuan), author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
Description:	1 online resource (11 pages) : illustrations.
Language:	English
Series:	NASA-TM ; 112019 NASA technical memorandum ; 112019.
Subject:	Airfoils. Computational fluid dynamics. High Reynolds number. Leading edges. Prediction analysis techniques. Aerofoils. Computational fluid dynamics.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11288396

Hidden Bibliographic Details
Other authors / contributors:	Dominik, C. J., author. American Institute of Aeronautics and Astronautics. United States. National Aeronautics and Space Administration, issuing body.
Notes:	"AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA." "AIAA 95-1858." Includes bibliographical references (page 11). Description based on online resource; title from PDF title page (NASA, viewed June 23, 2017).
Other form:	Print version: Optimization of an advanced design three-element airfoil at high reynolds numbers Microfiche version: Lin, J. C. Optimization of an advanced design three-element airfoil at high reynolds numbers
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:112019

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