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NASA Technical Note [NASA TN D-384]: Combinations of shear, compressive thermal, and compressive load stresses for the onset of permanent buckles in plates

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: NASA 1960 WashingtonDescription: 26pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-381 to 390	Not for loan		TR15587

Total holds: 0

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Previous	Hypersonic aerodynamics charectristics of minimum wave drag bodies having variations in cross sectional shape [NASA TN D-4079]	NASA Technical Note [NASA TN D-382]: Effect of blade cutout on power required by helicopters operating at high tip-speed ratios	NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges	NASA Technical Note [NASA TN D-384]: Combinations of shear, compressive thermal, and compressive load stresses for the onset of permanent buckles in plates	NASA Technical Note [NASA TN D-386]: Statistical data on control motions and airplane response of a republic F-84F airplane during operational training missions	NASA Technical Note [NASA TN D-388]: Transonic performance characteristics of several jet noise suppressors	NASA Technical Note [NASA TN D-389]: The longitudinal aerodynamic characteristics of a sweptback wing-body combination with and without end plates at mach numbers from 0.40 to 0.93	Next

Bound together NASA TN D-381 to 390

Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

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