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
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