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The effect of edge constraint on the buckling of sandwich and string-stiffened 120 degree conical shells subjected to external pressure [NASA CR-795]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. NASA 1967Description: 24p.Subject(s): Edge constraint

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR11906 [CR-795]

Total holds: 0

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Previous	AN INVESTIGATION OF THE FINE-POINTING CONTROL SYSTEM OF A SOFT-GIMBALED ORBITING TELESCOPE.	Stop-A computer program for supersonic transport trajectory optimization [NASA CR-793]	Environmental testing of contaminant producing materials from the integrated life support system [NASA CR-794]	The effect of edge constraint on the buckling of sandwich and string-stiffened 120 degree conical shells subjected to external pressure [NASA CR-795]	LABORATORY INVESTIGATION OF DIFFARACTION AND REFELECTION OF SONIC BOOMS BY BUILDINGS.	Parametric study of advanced multistage axial -flow compressors [NASA CR - 797] [Bound Contains NASA CR-797]	Cratering in low-density targets {NASA CR - 789] [Bound Contains NASA CR -796-800 ]	Next

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