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Experimental determination of the recovery factor and analytical solution of the conical flow field for a 20 degree included angle cone at mach numbers of 4.6 and 6.0 and stagnation tempratures to 2600 degree R [NASA TN D-353]

By: Pfyl, Frank A.
Contributor(s): Presley, Leroy L.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration. Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Description: 64p.Subject(s): Recovery factor
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Item type Current location Collection Call number Status Date due Barcode Item holds
Reference Reference PK Kelkar Library, IIT Kanpur
COMPACT STORAGE (BASEMENT) Not for loan 63658 [D-353]
Total holds: 0

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