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NASA Technical Note [NASA TN D-1949]: Flutter of flat rectangular orthotropic panels with biaxial loading and arbitrary flow direction

By: Washington. National Aeronautics and Space Administration (NASA).

Contributor(s): Bohon, Herman L.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1963Description: 33p.Subject(s): Aerodynamics, Supersonic

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-1941 to 1950	Not for loan		TR10699

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

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Previous	NASA Technical Note [NASA TN D-1946]: Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle	NASA Technical Note [NASA TN D-1947]: Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0 [degree] to 90 [degree]	NASA Technical Note [NASA TN D-1948]: Application of transtability concept to flutter of finite panels and experimental results	NASA Technical Note [NASA TN D-1949]: Flutter of flat rectangular orthotropic panels with biaxial loading and arbitrary flow direction	NASA Technical Note [NASA TN D-1950]: Random deviations from stabilized cruise altitudes of commercial transports at altitudes up to 40,000 feet with autopilot in altitude hold	Large-scale wind-tunnel investigation to improve the low-speed longitudinal stability at high lift of a supersonic transport with variable-sweep wings [NASA TN D-5005]	View factors for toroids and their parts [NASA TN D-5006]	Next

Bound together NASA TN D-1941 to 1950

Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

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