Comparison of wind-tunnel test results at M(infinity) = 0.7 with results from the boeing tea-230 subsonic flow method

Contributor(s): 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 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 2554 : 1975 Not for loan A32376
Total holds: 0

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