Add to ORKGA series of interdisciplinary modeling and analysis techniques that were specialized to address thre...
The Turbine Engine Hot Section Technology (HOST) Project of the NASA Lewis Research Center sponsored...
One of the significant ways in which the performance level of aircraft turbine engines has been impr...
Burner rig tests on simulated turbine blades, with and without internal cooling, to predict thermal ...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
An air-cooled turbine blade from an aircraft gas turbine engine chosen for its history of cracking w...
Presentations were made concerning the hot section environment and behavior of combustion liners, tu...
The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Sectio...
Steady state and transient conditions in creep and fatigue stress analysis of cooled turbine blade
Experimental data are presented for the tangential and radial stresses in the disks of the 36,000 ho...
Presentations were made concerning the development of design analysis tools for combustor liners, tu...
The effects of gas pressure level, coolant temperature, and coolant flow rate on the stress-strain h...
LecturePg. 31-44The disks and shafts of large steam turbines are subject to cracking from a variety ...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Experimental data are presented for the tangential and radial stresses in the disks of the 36,000 ho...
A series of interdisciplinary modeling and analysis techniques that were specialized to address thre...
The Turbine Engine Hot Section Technology (HOST) Project of the NASA Lewis Research Center sponsored...
One of the significant ways in which the performance level of aircraft turbine engines has been impr...
Burner rig tests on simulated turbine blades, with and without internal cooling, to predict thermal ...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
An air-cooled turbine blade from an aircraft gas turbine engine chosen for its history of cracking w...
Presentations were made concerning the hot section environment and behavior of combustion liners, tu...
The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Sectio...
Steady state and transient conditions in creep and fatigue stress analysis of cooled turbine blade
Experimental data are presented for the tangential and radial stresses in the disks of the 36,000 ho...
Presentations were made concerning the development of design analysis tools for combustor liners, tu...
The effects of gas pressure level, coolant temperature, and coolant flow rate on the stress-strain h...
LecturePg. 31-44The disks and shafts of large steam turbines are subject to cracking from a variety ...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Experimental data are presented for the tangential and radial stresses in the disks of the 36,000 ho...
A series of interdisciplinary modeling and analysis techniques that were specialized to address thre...
The Turbine Engine Hot Section Technology (HOST) Project of the NASA Lewis Research Center sponsored...
One of the significant ways in which the performance level of aircraft turbine engines has been impr...