The problem of crack growth in hot path components such as combustor liners is complicated by several practical and theoretical considerations. The loading environment of such components involves high temperature levels and gradients that lead to considerations such as thermal stresses, crack closure, hold time, inelastic strains (both time dependent and independent), and Thermal Mechanical Fatigue (TMF). In general, a good understanding of the influence of these factors on crack growth was not obtained. At the same time, several nonlinear fracture mechanics parameters were suggested for such applications; however, most of the proposed methods were not tested for broad applications such as required for hot section components. It was the pur...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
A major objective of the fatigue and fracture efforts under the Hot Section Technology (HOST) progra...
It is necessary to relate the processes that control crack growth in the immediate vicinity of the c...
The objective of the Elevated Temperature Crack Growth Program is to evaluate proposed nonlinear fra...
This paper is a summary of two NASA contracts on high temperature fatigue crack propagation in metal...
The purpose is to determine the ability of currently available P-I integrals to correlate fatigue cr...
Alloy 718 crack growth experiments were conducted to assess the ability of the selected path-indepen...
The purpose of this program was to extend the work performed in the base program (CR 182247) into th...
The objective of the Elevated Temperature Crack Growth Project is to evaluate proposed nonlinear fra...
A study was performed to examine the applicability of path-independent (P-I) integrals to crack grow...
The application of several fracture mechanics data correlation parameters to predicting the crack pr...
The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Sectio...
Hot section components of gas turbine engines are subject to severe thermomechanical loads during ea...
Three-dimensional, nonlinear, finite element structural analyses were performed for a simulated airc...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
A major objective of the fatigue and fracture efforts under the Hot Section Technology (HOST) progra...
It is necessary to relate the processes that control crack growth in the immediate vicinity of the c...
The objective of the Elevated Temperature Crack Growth Program is to evaluate proposed nonlinear fra...
This paper is a summary of two NASA contracts on high temperature fatigue crack propagation in metal...
The purpose is to determine the ability of currently available P-I integrals to correlate fatigue cr...
Alloy 718 crack growth experiments were conducted to assess the ability of the selected path-indepen...
The purpose of this program was to extend the work performed in the base program (CR 182247) into th...
The objective of the Elevated Temperature Crack Growth Project is to evaluate proposed nonlinear fra...
A study was performed to examine the applicability of path-independent (P-I) integrals to crack grow...
The application of several fracture mechanics data correlation parameters to predicting the crack pr...
The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Sectio...
Hot section components of gas turbine engines are subject to severe thermomechanical loads during ea...
Three-dimensional, nonlinear, finite element structural analyses were performed for a simulated airc...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
Thermally cycling a thin plate of nickel-based superalloy with an intense in-plane thermal gradient,...
A major objective of the fatigue and fracture efforts under the Hot Section Technology (HOST) progra...