Heat transfer on a flat plate in continuum to rarefied hypersonic flows at mach numbers of 19.2 and 25.4
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 onlineItem type | Current library | Call number | Status | Date due | Barcode | Item holds |
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Pamphlets Standards Reports | Central Library, IITB | LNASA CR 1692 : 1970 | Not for loan | A22126 |
Total holds: 0
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