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Achmed Schulz
Institut fuer Thermische Stroemungsmaschinen (ITS), Karlsruhe Institute of Technology (KIT), 76131 Karlsruhe, Germany
Obtenga más información sobre el autor en el Directorio de Especialistas
Articles
An Experimental Study of Airfoil and Endwall Heat Transfer on a Linear Turbine Blade Cascade Secondary Flow and Surface Roughness Effects
Vol. 41 '2010
-
Heat Transfer Research
Effect of Internal Rib Configurations on the Discharge Coefficient of a 30°-Inclined Film Cooling Hole
Vol. 41 '2010
-
Heat Transfer Research
Trailing Edge Film Cooling of Gas Turbine Airfoils Effects of Ejection Lip Geometry on Film Cooling Effectiveness and Heat Transfer
Vol. 41 '2010
-
Heat Transfer Research
A Survey on Efforts in Heat and Mass Transfer Analysis in Aero Engine Secondary Air/Oil Systems
Vol. 0 '1992
-
ICHMT DIGITAL LIBRARY ONLINE
Comparative Study of Low-Reynolds Number
k-ε
Turbulence Models for Predicting Heat Transfer along Turbine Blades with Transition
Vol. 0 '1992
-
ICHMT DIGITAL LIBRARY ONLINE
Turbine Airfoil Heat Transfer under Simulated Wake Conditions
Vol. 0 '1992
-
ICHMT DIGITAL LIBRARY ONLINE
AN EXPERIMENTAL STUDY OF AIRFOIL AND ENDWALL HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE − SECONDARY FLOW AND SURFACE ROUGHNESS EFFECTS
Vol. 0 '2009
-
ICHMT DIGITAL LIBRARY ONLINE
EFFECT OF INTERNAL RIB CONFIGURATIONS ON THE DISCHARGE COEFFICIENT OF A 30-DEG INCLINED FILM COOLING HOLE
Vol. 0 '2009
-
ICHMT DIGITAL LIBRARY ONLINE
TRAILING EDGE FILM COOLING OF GAS TURBINE AIRFOILS – EFFECTS OF EJECTION LIP GEOMETRY ON FILM COOLING EFFECTIVENESS AND HEAT TRANSFER
Vol. 0 '2009
-
ICHMT DIGITAL LIBRARY ONLINE
EFFUSION COOLED COMBUSTOR LINERS OF GAS TURBINES -AN ASSESSMENT OF THE CONTRIBUTIONS OF CONVECTIVE, IMPINGEMENT, AND FILM COOLING
Vol. 0 '2000
-
Proceedings of Symposium on Energy Engineering in the 21
st
Century (SEE2000) Volume I-IV
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