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NASA Technical Note [NASA TN D-543]: Fatigue-crack propagation in aluminum-alloy tension panels

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: NASA 1960 WashingtonDescription: 25pSubject(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-541 -50	Not for loan		TR15855

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	Saturn vehicle attitude resolver computer error analysis [NASA TN D-1119]	Servo loop design for air bearing inertial components [NASA TN D-1120]	NASA Technical Note [NASA TN D-542]: Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor	NASA Technical Note [NASA TN D-543]: Fatigue-crack propagation in aluminum-alloy tension panels	NASA Technical Note [NASA TN D-544]: Measured base pressures on several twin rocket-nozzle configurations at mach numbers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins	NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0	NASA TT [F-299]	Next

Bound together NASA TN D-541 to 550

Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

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