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Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes
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Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes
ID:
3508856
Creatori:
(1413158) Nagamatsu, Henry T., -2006
...
(1413159) Duffy R. E
...