Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

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Bibliographic Details
Author / Creator:	Howlett, James T., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, September 1987.
Description:	1 online resource (74 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2731 NASA technical paper ; 2731.
Subject:	Aerodynamics, Transonic. Viscous flow. Unsteady flow (Aerodynamics) Oscillating wings (Aerodynamics) Boundary layer. Aerodynamics, Transonic. Boundary layer. Oscillating wings (Aerodynamics) Unsteady flow (Aerodynamics) Viscous flow.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11665610

Hidden Bibliographic Details
Other authors / contributors:	Bland, Samuel R., author. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. Langley Research Center.
Notes:	"September 1987." Prepared at Langley Research Center. Includes bibliographical references (page 13). Technical paper. Langley Research Center 505-63-21-01 L-16289 Description based on online resource, PDF version; title from title page (NASA, viewed July 20, 2018).
Other form:	Print version: Howlett, James T Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment Microfiche : Howlett, James T Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2731

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