Numerical investigation of the effect of rim seal on turbine aerodynamic design parameters and end wall flows in low-aspect ratio turbine
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Computer Science
Reference22 articles.
1. An experimental investigation of gas-turbine disk cooling system;Kobayashi;J Eng Gas Turbines Power – Trans ASME,1984
2. Chew JW, Dadkhah S, Turner AB. Rim sealing of rotor–stator wheelspace in the absence of external flow. J Turbomach – Trans ASME 1992;114(2):433–8.
3. Dadkhah S, Turner AB, Chew JW. Performance of radial clearance rim seals in upstream and downstream rotor–stator wheelspace. J Turbomach – Trans ASME 1992;114(2):439–45.
4. Mclean C, Camci C, Glezer B. Mainstream aerodynamic effects due to wheelspace coolant injection in a high-pressure turbine stage: Part I – aerodynamic measurements in the stationary frame. J Turbomach – Trans ASME 2001;123(4):687–96.
5. Mclean C, Camci C, Glezer B. Mainstream aerodynamic effects due to wheelspace coolant injection in a high-pressure turbine stage: Part II – aerodynamic measurements in the rotational frame. J Turbomach – Trans ASME 2001;123(4):697–703.
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