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Neasurement of aerodynamics heat transfer to a deflected trailing edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6 [NASA Tn D-250]

By: Chauvin, Leo T. and Buglia James J.
Contributor(s): Buglia James J.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. NASA June 1960Description: 18p.Subject(s): Aerodynamic heat transfer
Contents:
Technical note D-250
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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) Not for loan 63648 D-250
Total holds: 0

Technical note D-250

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