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Local pressure distribution on a blunt delta wing for angles of attack up to 35(degre) at mach numbers of 3.4 and 4.7 [ NASA TN D-1554 ]

By: Kussoy, Marvin.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1962Description: 21p.Subject(s): Air jets | Turbulence
Contents:
NASA technical report
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
COMPACT STORAGE (BASEMENT) NASA TN D-1554 (Browse shelf) Not for loan TR15140
Total holds: 0

NASA technical report

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