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Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]

By: Bennett, Floyd V.
Material type: materialTypeLabelBookSeries: National Aeronautics and Spce Administratio (NASA). Publisher: Nasa, Washington, D.C. 1961Description: 41p.Subject(s): Aeroelastic
Contents:
Technical Note D-974
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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 TR13289 [TN D-974]
Total holds: 0

Bound With Nasa Tn D-971-973,975-980

Technical Note D-974

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