Effect of film-hole shape on turbine blade heat transfer coefficient distribution
38th Aerospace Sciences Meeting and Exhibit ; 2000 ; Reno , NV , U.S.A.
2000-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Film Injection Location on Local Heat Transfer Coefficient on a Gas Turbine Blade
Online Contents | 1998
|Turbine Blade Platform, Blade Tip and Shroud Heat Transfer
British Library Conference Proceedings | 1995
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