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An experimental study of the flutter of sails having a a delta planform tested from a macnh number of 0.1 to A mach number of 1.9 [NASA TM X-355]

By: Hess, Robert W.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D. C National Aeronautics and Space Administration 1961Description: 39p.Subject(s): Delta platform
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Item type Current location Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
Not for loan 102481 [X-355]
Total holds: 0

Bound vol. contains NASA TM X 350-396

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