11 research outputs found
Adiabatic Effectiveness and Heat Transfer Coefficient of Shaped Film Cooling Holes on a Scaled Guide Vane Pressure Side Model
Adiabatic Effectiveness and Heat Transfer Coefficient of Shaped Film Cooling Holes on a Scaled Guide Vane Pressure Side Model
The demand of improved thermal efficiency and high power output of modern gas turbine engines leads to extremely high turbine inlet temperature and pressure ratios. Sophisticated cooling schemes including film cooling are widely used to protect the vanes and blades of the first stages from failure and to achieve high component lifetimes.
In film cooling applications, injection from discrete holes is commonly used to generate a coolant film on the blade's surface
Internal Bearing Chamber Wall Heat Transfer as a Function of Operating Conditions and Chamber Geometry
Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes With Varying Angles of Inclination and Orientation
Festreden : Ansprachen bei der Feier des sechzigsten Geburtstags von Rektor Prof. Dr. Günter Pritschow. Abschiedsvorlesung von Altrektor Prof. Dr. Franz Effenberger
Inhalt: Ansprachen bei der Feier des sechzigsten Geburtstags von Rektor Prof. Dr. Günter Pritschow (Klaus R. G. Hein; Klaus von Trotha; Marcus Bierich; Sigmar Wittig; Horst Mehrländer; Michael Lateier; Franz Effenberger; Hans Klingel; Günter Pritschow: Danksagung) / Abschiedsvorlesung von Altrektor Prof. Dr. Franz Effenberger (Günter Pritschow: Begrüßung; Franz Effenberger: Abschiedsvorlesung - Was haben Bopserbrunnen, Blutfarbstoff und Perlonstrümpfe gemeinsam? Porträts dreier Stuttgarter Chemiker