Analysis of computed flow parameters for a set of sudden stalls in low-speed two-dimensional flow
Language: English Series: NASA TN D 85 : 1959Publication details: Washington, D.C. ; National Aeronautics and Space Administration ; 1959Edition: Description: 24 p; ISBN: Subject(s): | Flow subsonic, Flow laminar, Flow turbulent, Boundary layer-wing section, StallingOnline 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 TN D 85 : 1959 | Not for loan | A21833 |
Total holds: 0
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