Heat transfer on a flat plate in continuum to rarefied hypersonic flows at mach numbers of 19.2 and 25.4

Contributor(s): Language: English Series: NASA CR 1692 : 1970Publication details: Washington, D.C. ; National Aeronartics and Space Administration ; 1970Edition: Description: 55 p; ISBN: Subject(s): | Surface heat transfer, Flat plate, Hypersonic continuum, Free molecule flowOnline resources: Click here to access online
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Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA CR 1692 : 1970 Not for loan A22126
Total holds: 0

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