Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

Contributor(s): Language: English Series: NASA TP 2588 : 1987Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1987Edition: Description: 124 p; ISBN: Subject(s): | Nozzle-afterbody flow interactions, Reynolds number effects, Wind tunnel and flight comparisonOnline resources: Click here to access online
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Holdings
Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA TP 2588 : 1987 Not for loan A54977
Total holds: 0

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