Add to ORKGGeneral computer program for calculating axisymmetric temperature field applied to gas turbine face seal thermal deformatio
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
A computer program to calculate transient and steady state temperatures, pressures, and coolant flow...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Computer program analyzes the flow /leakage/ across a sealing dam for the case of steady, laminar, s...
FEATS computer code uses finite element analysis to calculate steady state temperature and thermal s...
A ceramic/metallic aircraft gas turbine outer gas path seal designed for improved engine performance...
Computer program for analysis of compressible fluid flow across sealing dam consisting of two closel...
The purposes of the computer tools for face seal analysis are new product optimization, existing sea...
Computer program for steady laminar, subsonic, and isothermal compressible flow across sealing da
A ceramic/metallic aircraft gas turbine outer gas path seal designed to enable improved engine perfo...
Coupled computer code for transient thermal response and ablation of noncharring heat shields and no...
Surface temperature mapping with infrared photographic pyrometry for turbine cooling investigation
A two dimensional finite difference numerical technique is presented to determine the temperature di...
A computer program to calculate the temperature profile of a flame or hot gas was presented in detai...
A computer program to calculate transient and steady state temperatures, pressures, and coolant flow...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
A computer program to calculate transient and steady state temperatures, pressures, and coolant flow...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade
Computer program analyzes the flow /leakage/ across a sealing dam for the case of steady, laminar, s...
FEATS computer code uses finite element analysis to calculate steady state temperature and thermal s...
A ceramic/metallic aircraft gas turbine outer gas path seal designed for improved engine performance...
Computer program for analysis of compressible fluid flow across sealing dam consisting of two closel...
The purposes of the computer tools for face seal analysis are new product optimization, existing sea...
Computer program for steady laminar, subsonic, and isothermal compressible flow across sealing da
A ceramic/metallic aircraft gas turbine outer gas path seal designed to enable improved engine perfo...
Coupled computer code for transient thermal response and ablation of noncharring heat shields and no...
Surface temperature mapping with infrared photographic pyrometry for turbine cooling investigation
A two dimensional finite difference numerical technique is presented to determine the temperature di...
A computer program to calculate the temperature profile of a flame or hot gas was presented in detai...
A computer program to calculate transient and steady state temperatures, pressures, and coolant flow...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
A computer program to calculate transient and steady state temperatures, pressures, and coolant flow...
Test rig for predicting thermal stress cracking in turbine stator or rotor blade