Computer program, TACTI, has been developed to calculate transient and steady-state temperatures, pressures, and flow in cooled turbine blade or vane with impingement insert. Coolant-side heat-transfer coefficients are calculated internally in program, with user specifying 1 of 3 modes of heat transfer at each station: impingement (including effect of crossflow); or forced convection over pin fins.
Analysis of a cooled, turbine blade or vane with an insert
NASA Tech Briefs ; 5 , 3
1981-01-01
Miscellaneous
No indication
English
Film Cooling of Insert Turbine Vane Trailing Edges
AIAA | 1972
|Cyclic stress analysis of an air-cooled turbine vane
TIBKAT | 1975
|Aircraft gas turbine blade and vane repair
Tema Archive | 1988
|BLADE OR VANE - DIMENSIONING OF TURBINE ENGINE AIRFOIL
SAE Technical Papers | 1996