Circumferentially smeared computed effects of rim seal clearance on wheelspace thermal distributions

Journal of Turbomachinery

Volumn 119, Issue 1, 1997, Pages 157-159

  Ko, S H ^a   Rhode, D L ^b   Guo, Z ^c  

^a Chungnam National University   (South Korea)

^b Department of Electrical and Computer Engineering   (United States)

^c EGS Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FINITE VOLUME METHOD; HEAT TRANSFER; HEATING; ORIFICES; ROTORS; STATORS; TURBULENT FLOW;

FINITE VOLUME COMPUTER CODE; HOT GAS INGRESS HEATING; INGRESS HEATING EFFECT; PURGE COOLANT FLOW; RIM SEAL CLEARANCE; TURBINE WHEELSPACE CAVITY; WHEELSPACE THERMAL DISTRIBUTIONS;

TURBOMACHINERY;

EID: 0030736414     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841005     Document Type: Article

References (3)

1. Hendricks, R., 1994, personal communication.
2. Ko, S. H., and Rhode, D. L., 1992, “Thermal Details in a Rotor-Stator Cavity at Engine Conditions With a Mainstream,” ASME Journal of Turbomachinery, Vol. 114, pp. 446-453.
3. Patankar, S. V., 1980, Numerical Heat Transfer and Fluid Flow, McGraw-Hill, New York.