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A STUDY OF FATIGUE AND FRACTURE IN 7075-T6 ALUMINUM ALLOY IN VACUUM AND AIR ENVIRONMENTS

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BookPublisher: Nasa, Washington, D.C. 1973Description: 36.DDC classification: NASA | TN D-7262

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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-7262 (Browse shelf)	Not for loan		TR12701

Total holds: 0

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Previous	NASA TN D-7259 COMPATIBILITY TESTS OF MATERIALS FOR A LITHIUM-COOLED SPACE POWER REACTOR CONCEPT	NASA TN D-7260 ANALYSIS OF HEAT TRANSFER FOR A NORMALLY IMPINGING LIQUID-METAL SLOT JET	NASA TN D-7261 PITTING FATIGUE CHARACTERISTICS OF AISI M-50 AND SUPER NITRALLOY SPUR GEARS	NASA TN D-7262 A STUDY OF FATIGUE AND FRACTURE IN 7075-T6 ALUMINUM ALLOY IN VACUUM AND AIR ENVIRONMENTS	NASA TN D-7263 A STUDY OF ZODIACAL LIGHT MODELS	NASA TN D-7264 AUTOMATED PROCEDURE FOR DESIGN OF WING STRUCTURES TO SATISFY STRENGHT AND FLUTTER REQUIREMENTS	NASA TN D-7265 GAS-PHASE HYDROGEN PERMEATION THROUGH ALPHA IRON,4130 STEEL, AND 304 STAINLESS STEEL FROM LESS THAN 100(DEGRE) C TO NEAR 600 (DEGRE) C	Next

Bound With Nasa Tn D-7250-7261,7263-7269 Lack No. 7251,7258

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