Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 /

Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 /

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Bibliographic Details
Author / Creator:Dearing, J. David, author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, April 1969.
Description:1 online resource (20 pages) : illustrations.
Language:English
Series:NASA technical note ; NASA TN D-5146
NASA technical note ; D-5146.
Subject:
Cone -- Hypersonic aerodynamics.
Laminar flow.
Aerodynamic heating.
Heat -- Transmission.
Space vehicles -- Thermodynamics.
Aerodynamic heating.
Cone -- Hypersonic aerodynamics.
Heat -- Transmission.
Laminar flow.
Space vehicles -- Thermodynamics.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12670477
Hidden Bibliographic Details
Other authors / contributors:United States. National Aeronautics and Space Administration, issuing body.
Notes:"April 1969."
Includes bibliographical references (page 9).
Description based on online resource, PDF version; title from title page (NASA, viewed on Oct. 26, 2020).
Other form:Print version: Dearing, J. David Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10
GPO item no.:0830-H-13 (online)
Govt.docs classification:NAS 1.14:D-5146

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