Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /

Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /

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Bibliographic Details
Author / Creator:	Jones, Kenneth M., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
Description:	1 online resource (25 pages) : illustrations.
Language:	English
Series:	NASA-TM ; 112005 NASA technical memorandum ; 112005.
Subject:	Aerodynamic configurations. Airfoils. Computational fluid dynamics. Navier-Stokes equation. Reynolds number. Wing flaps. Aerofoils. Computational fluid dynamics. Reynolds number.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11288384

Hidden Bibliographic Details
Other authors / contributors:	Biedron, Robert T., author. Whitlock, Mark, author. American Institute of Aeronautics and Astronautics. United States. National Aeronautics and Space Administration, issuing body.
Notes:	"13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California." "AIAA 95-1855." Includes bibliographical references (page 12). Description based on online resource; title from PDF title page (NASA, viewed June 22, 2017).
Other form:	Print version: Application of a navier-stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques Microfiche version: Jones, Kenneth M. Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:112005

Description
Item Description:	"13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California." "AIAA 95-1855."
Physical Description:	1 online resource (25 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 12).