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INVESTIGATION OF FATIGUE CRACK GROWTH IN TI-8A1-1M0-1V (DUPLEX-ANNEALED) SPECIMENS HAVING VARIOUS WIDTHS.

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BookPublisher: Nasa, Washington, D.C. 1967Description: 10.DDC classification: NASA | TN D-3879

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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-3879 (Browse shelf)	Not for loan		TR10549

Total holds: 0

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Previous	NASA TN D-3876 TECHNIQUE FOR VERIFYING STRUCTURAL INTEGRITY OF FULL-SCALE SEGMENTS OF LAUNCH VEHICLES AT TRANSONIC SPEEDS.	NASA TN D-3877 THE AXIALLY SYMMETRIC RESPONSE OF AN ELASTIC CYLINDRICAL SHELL PARTIALLY FILLED WITH LIQUED.	NASA TN D-3878 EFFECTIVENESS OF FLEXIBLE AND RIGID RING BAFFLRS FOR DAMPING LIQUID OSCILATIONS IN LARGE-SCALE CYLINDERICAL TANKS.	NASA TN D-3879 INVESTIGATION OF FATIGUE CRACK GROWTH IN TI-8A1-1M0-1V (DUPLEX-ANNEALED) SPECIMENS HAVING VARIOUS WIDTHS.	NASA TN D3880 PLASMA STABILITY AND THE BOHR-VAN LEEUWEN THEOREM.	NASA TN D-3892 CONTRIBUTION OF DOWNSTREAM STATOR TO THE INTERACTION NOISE OF SINGLE-STAGE AXIAL-FLOW COMPRESSOR	NASA TN D-3893 A NUMERICAL METHOD FOR DETERMINING THE AEROELASTIC DIVERGENCE CHARACTERISTICS OF UNGUIDED, SLENDER-BODY, MULTISTAGE LAUNCH VEHICLES	Next

Bound With Nasa Tn D-3871-78 And D-3880

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