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Achmed Schulz
Institut fuer Thermische Stroemungsmaschinen (ITS), Karlsruhe Institute of Technology (KIT), 76131 Karlsruhe, Germany
Obtenha mais informações sobre o autor no Diretório 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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