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DETERMINATION OF THE CREEP DEFLECTION AND LIFETIME OF ALUMINUM-ALLOY MULTIWEB BOX BEAMS SUBJECTED TO VERIED LOADS AT CONSTANT TEMPERATURE

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BookPublisher: Nasa, Washington, D.C. 1962Description: 33.DDC classification: NASA | TN D-1265

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1265 (Browse shelf)	Not for loan		TR13022

Total holds: 0

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Previous	NASA TN D-1262 STATISTICAL STUDY OF EFFECTS OF INSERTION ERRORS ON ASCENT TRAJECTORIES FOR LUNAR MISSIONS	NASA TN D-1263 EFFECTS OF FOREBODY LENGTH ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING	NASA TN D-1264 PRESSURE DISTRIBUTIONS AT MACH NUMBER 2.05 ON A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER	NASA TN D-1265 DETERMINATION OF THE CREEP DEFLECTION AND LIFETIME OF ALUMINUM-ALLOY MULTIWEB BOX BEAMS SUBJECTED TO VERIED LOADS AT CONSTANT TEMPERATURE	NASA TN D-1266 INDUCED PRESSURES ON CYLINDRICAL RODS WITH VARIOUS NOSE DRAGS AND NOSE SHAPES AT MACH NUMBERS OF 17 AND 21	NASA TN D-1267 CURRENT ESTIMATES OF RADIATION DOES IN SPACE	NASA TN D-1268 MEASUREMENT OF TOTAL NORMAL EMITTANCE OF BORON NITRIDE FROM 1,200 (DEGRE) F TO 1,900 (DEGRE) F WITH NORMAL SPECTRAL EMITTANCE DATA AT 1,400 (DEGRE) F	Next

Bound With Nasa Tn D-1261-1264,1266-1270

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