Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal mach number of 7
Language: English Series: NASA TP 2307 : 1985Publication details: Washington, D.C. ; National Aeronautics and Space Administration ; 1985Edition: Description: 48 p; ISBN: Subject(s): | Space shuttle, Hypersonic flow, Thermal protection, Reusable surface, Impingement heatingOnline resources: Click here to access online| Item type | Current library | Call number | Status | Date due | Barcode | Item holds |
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Pamphlets Standards Reports
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Central Library, IITB | LNASA TP 2307 : 1985 | Not for loan | A54022 |
Total holds: 0
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