Room-temperature static and cyclic tests were made on 21 aluminum plates in the shape of a 91.4x91.4-cm Maltese cross with 45 deg flaws to develop crack growth and fracture toughness data under mixed-mode conditions. During cyclic testing, it was impossible to maintain a high proportion of shear-mode deformation on the crack tips. Cracks either branched or turned. Under static loading, cracks remained straight if shear stress intensity exceeded normal stress intensity. Mixed-mode crack growth rate data compared reasonably well with published single-mode data, and measured crack displacements agreed with the straight and branched crack analyses. Values of critical strain energy release rate at fracture for pure shear were approximately 50% h...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
An experimental study was conducted to determine the effects of combined bending and membrane cyclic...
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
This experimental program was undertaken to determine the effects of combined cyclic/sustained loads...
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
Static fracture tests were performed on surface flawed specimens of aluminum and titanium alloys. A ...
Recommendations are given for the design, preparation, and static fracture testing of surface crack ...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
A program was conducted to determine the fatigue-crack propagation behavior of parent and welded 221...
This paper is a summary of two NASA contracts on high temperature fatigue crack propagation in metal...
The fatigue crack propagation behavior of two commercial Al alloys was studied using spectrum loadin...
The variables studied in the stress-corrosion cracking performance of high strength aluminum alloys ...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
An experimental study was conducted to determine the effects of combined bending and membrane cyclic...
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
This experimental program was undertaken to determine the effects of combined cyclic/sustained loads...
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
Static fracture tests were performed on surface flawed specimens of aluminum and titanium alloys. A ...
Recommendations are given for the design, preparation, and static fracture testing of surface crack ...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
A program was conducted to determine the fatigue-crack propagation behavior of parent and welded 221...
This paper is a summary of two NASA contracts on high temperature fatigue crack propagation in metal...
The fatigue crack propagation behavior of two commercial Al alloys was studied using spectrum loadin...
The variables studied in the stress-corrosion cracking performance of high strength aluminum alloys ...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
An experimental study was conducted to determine the effects of combined bending and membrane cyclic...
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature