Add to ORKGThe effects of gas pressure level, coolant temperature, and coolant flow rate on the stress-strain history and life of an air-cooled vane were analyzed using measured and calculated transient metal temperatures and a turbine blade stress analysis program. Predicted failure locations were compared to results from cyclic tests in a static cascade and engine. The results indicate that a high gas pressure was detrimental, a high coolant flow rate somewhat beneficial, and a low coolant temperature the most beneficial to vane life
ABSTRACT: To be able to design next generation of gas turbines it is necessary to improve the knowle...
During operation, gas turbine components undergo various types of timedependent degradation due to ...
Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...
Experimental transient turbine vane metal temperatures were obtained from tests conducted on air-coo...
Steady state and transient conditions in creep and fatigue stress analysis of cooled turbine blade
The creep fatigue behavior of a fully impingement cooled blade for four cyclic cases was analyzed by...
Seventy-two air-cooled turbine vanes were tested to determine coolant flow variations among the vane...
Coolant pressure and flow distribution through air cooled vane for high temperature gas turbin
An experimental heat transfer investigation was conducted on an air-cooled turbine vane made from wi...
ABSTRACT: The analysis of stress values that are produced while the turbine is running are the key f...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Convection cooled turbine vane metal wall temperatures experimentally obtained in a hot cascade for ...
Experimental temperatures are presented for an air-cooled turbine rotor blade tested in an engine. T...
The most critical structural requirements that aircraft gas turbine engines must meet result from th...
The heat-transfer characteristics of a chordwise-finned, impingement-cooled vane were investigated i...
ABSTRACT: To be able to design next generation of gas turbines it is necessary to improve the knowle...
During operation, gas turbine components undergo various types of timedependent degradation due to ...
Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...
Experimental transient turbine vane metal temperatures were obtained from tests conducted on air-coo...
Steady state and transient conditions in creep and fatigue stress analysis of cooled turbine blade
The creep fatigue behavior of a fully impingement cooled blade for four cyclic cases was analyzed by...
Seventy-two air-cooled turbine vanes were tested to determine coolant flow variations among the vane...
Coolant pressure and flow distribution through air cooled vane for high temperature gas turbin
An experimental heat transfer investigation was conducted on an air-cooled turbine vane made from wi...
ABSTRACT: The analysis of stress values that are produced while the turbine is running are the key f...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Convection cooled turbine vane metal wall temperatures experimentally obtained in a hot cascade for ...
Experimental temperatures are presented for an air-cooled turbine rotor blade tested in an engine. T...
The most critical structural requirements that aircraft gas turbine engines must meet result from th...
The heat-transfer characteristics of a chordwise-finned, impingement-cooled vane were investigated i...
ABSTRACT: To be able to design next generation of gas turbines it is necessary to improve the knowle...
During operation, gas turbine components undergo various types of timedependent degradation due to ...
Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...