Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /

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Bibliographic Details
Author / Creator:	Hamilton, H. Harris, author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, August 1968.
Description:	1 online resource (44 pages) : illustrations.
Language:	English
Series:	NASA technical note ; TN D-4686 NASA technical note ; D-4686.
Subject:	Boundary layer control. Flaps (Airplanes) Wedges. Aircraft separation. Aircraft separation. Boundary layer control. Flaps (Airplanes) Wedges.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12691619

Hidden Bibliographic Details
Other authors / contributors:	Dearing, J. David, author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center.
Notes:	"August 1968." Includes bibliographical references (pages 18-21). Description based on online resource, PDF version; title from title page (NASA, viewed on Dec. 11, 2020).
Other form:	Print version: Hamilton, H. Harris Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-4686

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