EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION OF FLOW IN GAS TURBINE BLADE COOLING PASSAGES
Conference; 31st, Fluid dynamics; 31st AIAA ; 2001 ; Anaheim, CA
01.01.2001
ALL
Nos 2001-2700 to 2001-3095 with gaps held only
Aufsatz (Konferenz)
Englisch
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Designing Turbine Blade Internal Cooling Passages Using Response Surface and Kriging Methodologies
British Library Conference Proceedings | 2000
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