The intent of this program is to develop a basic understanding of cyclic creep-fatigue deformation mechanisms and damage accumulation, a capability for reliable life prediction, and the ability to model the constitutive behavior of anisotropic single crystal (SC) and directionally solidified or recrystallized (DSR) comprise the program, and the work breakdown for each option reflects a distinct concern for two classes of anisotropic materials, SC and DSR materials, at temperatures encountered in the primary gas path (airfoil temperatures), and at temperatures typical of the blade root attachment and shank area. Work directed toward the higher temperature area of concern in the primary gas path includes effects of coatings on the behavior an...
Turbine blades derived from directionally solidified (DS) Ni-base superalloys are increasingly emplo...
The overall objective of this program is to demonstrate the applicability of NASA-developed advanced...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
The purpose is to develop life prediction models for coated anisotropic materials used in gas temper...
The purpose of this program is to develop life prediction models for coated anisotropic materials us...
Work to develop fatigue life prediction and constitutive models for uncoated attachment regions of s...
Single crystal materials are being used in gas turbine airfoils and are candidates for other hot sec...
One of the primary drivers that prompted the initiation of the hot section technology (HOST) program...
Turbine blades for reusable space propulsion systems are subject to severe thermomechanical loading ...
A major objective of the fatigue and fracture efforts under the NASA Hot Section Technology (HOST) p...
Successful attempts were made to model the deformation behavior of nickel base superalloys to be use...
Directionally solidified (DS) nickel-base superalloys are used in high temperature gas turbine engin...
Drives to improve gas turbines efficiency have lead to an increase in firing temperatures. This incr...
The most critical structural requirements that aircraft gas turbine engines must meet result from th...
The achievement of high efficiency in large land-based stationary gas turbines for electric power ge...
Turbine blades derived from directionally solidified (DS) Ni-base superalloys are increasingly emplo...
The overall objective of this program is to demonstrate the applicability of NASA-developed advanced...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
The purpose is to develop life prediction models for coated anisotropic materials used in gas temper...
The purpose of this program is to develop life prediction models for coated anisotropic materials us...
Work to develop fatigue life prediction and constitutive models for uncoated attachment regions of s...
Single crystal materials are being used in gas turbine airfoils and are candidates for other hot sec...
One of the primary drivers that prompted the initiation of the hot section technology (HOST) program...
Turbine blades for reusable space propulsion systems are subject to severe thermomechanical loading ...
A major objective of the fatigue and fracture efforts under the NASA Hot Section Technology (HOST) p...
Successful attempts were made to model the deformation behavior of nickel base superalloys to be use...
Directionally solidified (DS) nickel-base superalloys are used in high temperature gas turbine engin...
Drives to improve gas turbines efficiency have lead to an increase in firing temperatures. This incr...
The most critical structural requirements that aircraft gas turbine engines must meet result from th...
The achievement of high efficiency in large land-based stationary gas turbines for electric power ge...
Turbine blades derived from directionally solidified (DS) Ni-base superalloys are increasingly emplo...
The overall objective of this program is to demonstrate the applicability of NASA-developed advanced...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...