Add to ORKGThe low-cycle, creep-fatigue characteristics of the advanced gas turbine disk alloy, AF2-1DA have been determined at 1400 F and are presented in terms of the method of strainrange partitioning (SRP). The mean stresses which develop in the PC and CP type SRP cycles at the lowest inelastic strainrange were observed to influence the cyclic lives to a greater extent than the creep effects and hence interfered with a conventional interpretation of the results by SRP. A procedure is proposed for dealing with the mean stress effects on life which is compatible with SRP
The basic concepts of strain range partitioning are reviewed and the areas requiring for expanded ve...
An updated procedure for characterizing an alloy and predicting cyclic life by using the total strai...
The ultrahigh vacuum strain controlled thermal-mechanical strain cycling fatigue behavior of ASTAR 8...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
This report addresses Strainrange Partitioning, an advanced life prediction analysis procedure, as a...
Procedures are presented for characterizing an alloy and predicting cyclic life for isothermal and t...
Several nickel-base aircraft turbine disk superalloys were evaluated at 650 C for resistance to fati...
A study was made to assess the ability of the method of Strainrange Partitioning (SRP) to both corre...
Strainrange Partitioning provides unifying framework for characterizing high-temperature, low-cycle,...
The creep fatigue behavior of a fully impingement cooled blade for four cyclic cases was analyzed by...
Procedures are presented for expressing the Strainrange Partitioning (SRP) method for creep fatigue ...
The basic concepts of strain range partitioning are reviewed and the areas requiring for expanded ve...
An updated procedure for characterizing an alloy and predicting cyclic life by using the total strai...
The ultrahigh vacuum strain controlled thermal-mechanical strain cycling fatigue behavior of ASTAR 8...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
The military aircraft gas turbine engines are often required to undergo a complex set of.operating c...
This report addresses Strainrange Partitioning, an advanced life prediction analysis procedure, as a...
Procedures are presented for characterizing an alloy and predicting cyclic life for isothermal and t...
Several nickel-base aircraft turbine disk superalloys were evaluated at 650 C for resistance to fati...
A study was made to assess the ability of the method of Strainrange Partitioning (SRP) to both corre...
Strainrange Partitioning provides unifying framework for characterizing high-temperature, low-cycle,...
The creep fatigue behavior of a fully impingement cooled blade for four cyclic cases was analyzed by...
Procedures are presented for expressing the Strainrange Partitioning (SRP) method for creep fatigue ...
The basic concepts of strain range partitioning are reviewed and the areas requiring for expanded ve...
An updated procedure for characterizing an alloy and predicting cyclic life by using the total strai...
The ultrahigh vacuum strain controlled thermal-mechanical strain cycling fatigue behavior of ASTAR 8...