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Fatigue of notched Ti-8Al-1mo-1V titanium alloy at room temperature and 55o degree F (560 degree K) with Flight by flight loading representative of a supersonic transport [NASA TN D-5294]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration (NASA)Publication details: NASA 1969 Washington, D.CDescription: 42pSubject(s):

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NASA technical note D-5294

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR14382 [D-5294]

Total holds: 0

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Previous	Operational experiences of turbine-powered commercial transport airplanes [NASA TN D-1392]	Method for prediction of pump cavitation performance for various liquids, liquid temperatures, and rotative speeds [NASA TN D-5292]	Interplanetary probe missions with solar electric propulsion systems [NASA TN D-5293]	Fatigue of notched Ti-8Al-1mo-1V titanium alloy at room temperature and 55o degree F (560 degree K) with Flight by flight loading representative of a supersonic transport [NASA TN D-5294]	Description of high enthalpy arc tunnel at the langley research center including test-stream conditions at selected operating points [NASA TN D-5295]	Inflation and performance of three parachute configurations from supersonic flight tests in a low-density environment [D5296]	Flow-field measurement of two protuberances on a flat plate submerged in a turbulent boundary layer at mach 2.49 and 4.44 [NASA TN D-5297]	Next

NASA technical note D-5294

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