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21篇 您的检索式:作者名="Bolcs A"
    题名 作者 年代 出处 被引量
1Flow Characteristics in Two-Leg Internal Coolant Passages of Gas Turbine Airfoils With FilmCooling Hole Ejection显示文摘Chantetoup D Bolcs A 2002Journal of Turbomachinery2002,124,7:3
2Investigation of Detailed Film Cooling Effectiveness and Heat Transfer Distributions on a Gas Turbine Airfoil 显示文摘Drost U Bolcs A 1999Journal of Turbomachinery1999,,121:1
3Experimental study of showerhead cooling on a cylinder comparing several configurations using cylindrical and shaped holes显示文摘Reiss H Bolcs A 2000Journal of Turbomachinery2000,,122:1
4Experimental study of showerhead cooling on a cylinder comparing several configurations using cylindrical and shaped holes 显示文摘Reiss H Bolcs A 2000Journal of Turbomachinery2000,122,1:1
5Lo- calization of specific mRNAs in Xenopus embryos by whole-mount in situ hybridization 显示文摘Hemmati-Brivanlou A Frank D Bolce ME 1990Development1990,110,:1
6Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil显示文摘DROST U BOLCS A 1999ASME J of Turbomach1999,121,1:1
7Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil 显示文摘DROST U BOLCS A 1999ASME Journal of Turbomachinery1999,121,1:1
8Experimental Study of Shower Head Cooling on a Cylinder Comparing Several Configurations Using Cylindrical and Shaped Holes 显示文摘Reiss H Bolcs A 2000ASME Journal of Turbo Machinery2000,122,:1
9Heat transfer measurements on a turbine airfoil at various Reynolds numbers and turbulence intensities including effects of surface roughness显示文摘Hoffs A Drost U Bolcs A 1996ASME Paper 96-GT-1691996,,:1
10Flow Effects on the Bend Re- gion Heat Transfer Distribution of 2-Pass Internal Coolant Passages of Gas Turbine Airfoils: Influence of Film Cool- ing Extraction 显示文摘Chanteloup D Bolcs A 2003ASME Conference Proceedings2003,2003,36886:1
11Combined 3-D Flow and Heat Transfer Measurements in a 2-Pass Internal Coolant Passage of Oas Turbine Airfoils 显示文摘Chanteloup D Y Juaneda Bolcs A 2002Journal of Turbomachinery Transactions of the ASME2002,124,4:1
12Combined 3D flow and heat transfer measurements in a 2-pass internal coolant passage of gas turbine airfoils显示文摘Chanteloup D Juaneda Y Bolcs A 2002Journal of Turbomachinery2002,124,4:1
13Flow characteristics in two-leg internal coolant passage of gas turbine airfoils with film-cooling hole ejection显示文摘CHANTELOUP D BOLCS A 2002Journal of Turbomachinery of ASME2002,124,7:1
14Flow characteristics in two-leg in ternal coolant passages of gas turbine airfoils with film cooling hole ejection显示文摘Chanteloup D Bolcs A 2002ASME Journal of Turbomachinery2002,124,3:1
15Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil显示文摘DROST U BOLCS A 1999ASME Journal of Turbomachinery1999,121,:1
16Experimental study of showerhead cooling on a cylinder comparing several configurations using cylindrical and shaped holes显示文摘Reiss H Bolcs A 2000Journal of Turbomachinery2000,122,4:1
17Experimental study of showerhead cooling on a cylinder comparing several configurations using cylindrical and shaped holes显示文摘Reiss H Bolcs A 2000Journal of Turbomachincry2000,122,16:1
18Aeroelasticity in Turbomachinescomparison of Theoretical and Experimental Results 显示文摘Bolcs A Fransson T H 1986Communication du Laboratoire de Thermique Applique et de Turbomachines1986,,:1
19Investigation of Detailed Film Cooling Effectiveness and Heat Transfer Distributions on A Gas Turbine Airfoil 显示文摘Drost U Bolcs A 1999ASME Journal of Turbomachinery1999,121,:1
20Combined 3D flow and heat transfer measurements in a 2-pass internal coolant passage of gas turbine airfoils 显示文摘Chanteloup D Juaneda Y Bolcs A 2002ASME Journal of Torbomachinery2002,124,4:1
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