Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /

Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /

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Bibliographic Details
Author / Creator:	Hamilton, H. Harris, author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980.
Description:	1 online resource (75 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1698 NASA technical paper ; 1698.
Subject:	Axisymmetric flow. Inviscid flow. Laminar heat transfer. Streamlined bodies. Three dimensional boundary layer. Boundary layer. Laminar flow.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914286

Hidden Bibliographic Details
Other authors / contributors:	Langley Research Center. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 10, 2016). "September 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page. Includes bibliographical references (pages 40-42). Technical paper. National Aeronautics and Space Administration 506-51-13-01 L-13748
Other form:	Print version: Hamilton, H. Harris. Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue Microfiche version: Hamilton, H. Harris. Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1698

Description
Item Description:	Title from title screen (viewed on Aug. 10, 2016). "September 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:	1 online resource (75 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 40-42).