Comparison of wind-tunnel test results at M(infinity) = 0.7 with results from the boeing tea-230 subsonic flow method
Language: English Series: NASA CR 2554 : 1975Publication details: Washington, D.C. ; National Aeronartics and Space Administration ; 1975Edition: Description: 91 p; ISBN: Subject(s): | Potential flow analysis, Wind tunnel data, Pressure distribution, Test-theory comparison, Overwing nacelleOnline 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 2554 : 1975 | Not for loan | A32376 |
Total holds: 0
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