Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws Originating at Fastener Holes written by L. R. Hall and published by . This book was released on 1974 with total page 325 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws Originating at Fastener Holes written by L. R. Hall and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fracture and Fatigue Crack Growth Behavior written by L. R. Hall and published by . This book was released on 1974 with total page 351 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws Originating at Fastener Holes written by L. R. Hall and published by . This book was released on 1974 with total page 351 pages. Available in PDF, EPUB and Kindle. Book excerpt: The combined experimental and analytical study was undertaken to investigate the fatigue crack growth behavior of surface flaws and part-thru and thru cracks originating at fastener holes. Three alloys (2219-T851 aluminum, 9Ni-4Co-0.2C steel, and 6Al-4V (ELI) beta annealed titanium) were tested under three different loading profiles (constant cyclic load, periodic overload, spectrum load). Surface flaw test variables included loading conditions (uniform tension, pure bending, combined bending and tension), stress ratio (0. 1, 0.3, 0.5), initial flaw shape (0.15

Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws Originating at Fastener Holes written by L. R. Hall and published by . This book was released on 1974 with total page 325 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report contains tabulations of raw fatigue crack growth rate data generated during tests of surface flaws and flaws originating at fastener holes. The surface flaw tests involved a number of variables including alloy, flaw shape, initial flaw depth, loading profile, and stress ratio. Three alloys were tested including 2219-T851 aluminum, 9Ni-4Co-0.2C steel (190-210 ksi), and 6Al-4V standard ELI beta annealed titanium, all in plate form. Most specimens contained two or three flaws having initial depth-to-length ratios of 0.15, 0.30, or 0.45, and initial depth-to-thickness ratios ranging from 20 to 80 percent of the specimen thickness. Three different loading profiles were investigated including constant cyclic load, periodic overload, and spectrum loadings.

Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws Originating at Fastener Holes Volume II Tabulated Data written by L. R. Hall and published by . This book was released on 1974 with total page 325 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report contains tabulations of raw fatigue crack growth rate data generated during tests of surface flaws and flaws originating at fastener holes. The surface flaw tests involved a number of variables including alloy, flaw shape, initial flaw depth, loading profile, and stress ratio. Three alloys were tested including 2219-T851 aluminum, 9Ni-4Co-0.2C steel (190-210 ksi), and 6Al-4V standard ELI beta annealed titanium, all in plate form. Most specimens contained two or three flaws having initial depth-to-length ratios of 0.15, 0.30, or 0.45, and initial depth-to-thickness ratios ranging from 20 to 80 percent of the specimen thickness. Three different loading profiles were investigated including constant cyclic load, periodic overload, and spectrum loadings.

Download or read book Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws Originating at Fastener Holes Volume I Results and Discussion written by L. R. Hall and published by . This book was released on 1974 with total page 366 pages. Available in PDF, EPUB and Kindle. Book excerpt: The combined experimental and analytical study was undertaken to investigate the fatigue crack growth behavior of surface flaws and part-thru and thru cracks originating at fastener holes. Three alloys (2219-T851 aluminum, 9Ni-4Co-0.2C steel, and 6Al-4V (ELI) beta annealed titanium) were tested under three different loading profiles (constant cyclic load, periodic overload, spectrum load). Surface flaw test variables included loading conditions (uniform tension, pure bending, combined bending and tension), stress ratio (0.1, 0.3, 0.5), initial flaw shape (0.15

Download or read book NASA Technical Note written by and published by . This book was released on 1976 with total page 772 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fatigue Crack Growth under Spectrum Loads written by and published by ASTM International. This book was released on 1976 with total page 362 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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Download or read book Methods and Models for Predicting Fatigue Crack Growth Under Random Loading written by and published by ASTM International. This book was released on with total page 147 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book T I S C A Technical Information Indexes written by United States. Naval Air Systems Command and published by . This book was released on 1975 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fracture mechanics fifteenth symposium written by Melvin F. Kanninen and published by ASTM International. This book was released on with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Methods and Models for Predicting Fatigue Crack Growth Under Random Loading written by J. B. Chang and published by ASTM International. This book was released on 1981 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Fatigue Crack Growth Measurement and Data Analysis written by S. J. Hudak and published by ASTM International. This book was released on 1981 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Part Through Crack Fatigue Life Prediction written by J. B. Chang and published by ASTM International. This book was released on 1979 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt: