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

Saved in:
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:
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

MARC

LEADER 00000cam a2200000 i 4500
001 12670477
005 20201113090829.0
006 m o d f
007 cr |||||||||||
008 120408e196904 dcua obt f000 0 eng c
003 ICU
035 |a (OCoLC)785286727 
042 |a pcc 
040 |a OCLCE  |b eng  |e rda  |e pn  |c OCLCE  |d OCLCQ  |d OCLCF  |d OCLCQ  |d COP  |d GPO  |d MvI 
074 |a 0830-H-13 (online) 
086 0 |a NAS 1.14:D-5146 
100 1 |a Dearing, J. David,  |e author.  |0 http://id.loc.gov/authorities/names/no2008173923  |1 http://viaf.org/viaf/21972301 
245 1 0 |a Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 /  |c by J. David Dearing. 
264 1 |a Washington, D.C. :  |b National Aeronautics and Space Administration,  |c April 1969. 
300 |a 1 online resource (20 pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent  |0 http://id.loc.gov/vocabulary/contentTypes/txt 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier  |0 http://id.loc.gov/vocabulary/carriers/cr 
490 1 |a NASA technical note ;  |v NASA TN D-5146 
500 |a "April 1969." 
504 |a Includes bibliographical references (page 9). 
588 |a Description based on online resource, PDF version; title from title page (NASA, viewed on Oct. 26, 2020). 
650 0 |a Cone  |x Hypersonic aerodynamics. 
650 0 |a Laminar flow. 
650 0 |a Aerodynamic heating. 
650 0 |a Heat  |x Transmission. 
650 0 |a Space vehicles  |x Thermodynamics. 
650 7 |a Aerodynamic heating.  |2 fast  |0 (OCoLC)fst00798175 
650 7 |a Cone  |x Hypersonic aerodynamics.  |2 fast  |0 (OCoLC)fst01766857 
650 7 |a Heat  |x Transmission.  |2 fast  |0 (OCoLC)fst00953826 
650 7 |a Laminar flow.  |2 fast  |0 (OCoLC)fst00991079 
650 7 |a Space vehicles  |x Thermodynamics.  |2 fast  |0 (OCoLC)fst01128098 
710 1 |a United States.  |b National Aeronautics and Space Administration,  |e issuing body.  |0 http://id.loc.gov/authorities/names/n78087581  |1 http://viaf.org/viaf/146202023 
776 0 8 |i Print version:  |a Dearing, J. David  |t Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10  |w (OCoLC)50762830 
830 0 |a NASA technical note ;  |v D-5146. 
856 4 0 |u https://purl.fdlp.gov/GPO/gpo146477  |y Government Publishing Office 
903 |a HeVa 
903 |a HeVa 
929 |a eresource 
999 f f |i cb0144ae-3fcf-57ad-b326-362c7f36d9d4  |s b19ff110-b5d0-5035-a262-656ce61fd87a 
928 |t Library of Congress classification  |l Online  |c UC-FullText  |u https://purl.fdlp.gov/GPO/gpo146477  |z Government Publishing Office  |g ebooks  |i 12801715