期刊


ISSN0889-504X
刊名Journal of Turbomachinery
参考译名涡轮机械杂志
收藏年代1995～2024



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2001, vol.123, no.1 2001, vol.123, no.2 2001, vol.123, no.3 2001, vol.123, no.4

题名作者出版年年卷期
High Lift and Aft-Loaded Profiles for Low-Pressure TurbinesR. J. Howell; O. N. Ramesh; H. P. Hodson; N. W. Harvey20012001, vol.123, no.2
Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil ConditionsRalph J. Volino; Lennart S. Hultgren20012001, vol.123, no.2
Turbine Separation Control Using Pulsed Vortex Generator JetsJeffrey P. Bons; Rolf Sondergaard; Richard B. Rivir20012001, vol.123, no.2
Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the EndwallH. Sauer; R. Muller; K. Vogeler20012001, vol.123, no.2
An Experimental Study of the Effect of Wake Passing on Turbine Blade Film CoolingJames D. Heidmann; Barbara L. Lucci; Eli Reshotko20012001, vol.123, no.2
Film Cooling Downstream of a Row of Discrete Holes With Compound AngleR. J. Goldstein; P. Jin20012001, vol.123, no.2
Scaling of Performance for Varying Density Ratio Coolants on an Airfoil With Strong Curvature and Pressure Gradient EffectsMarcia I. Ethridge; J. Michael Cutbirth; David G. Bogard20012001, vol.123, no.2
Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1 - Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge CoefficientsOguz Uzol; Cengiz Camci; Boris Glezer20012001, vol.123, no.2
Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 2 - External Aerodynamics, Total Pressure Losses, and PredictionsOguz Uzol; Cengiz Camci20012001, vol.123, no.2
A Method for Correlating the Influence of External Crossflow on the Discharge Coefficients of Film Cooling HolesD. A. Rowbury; M. L. G. Oldfield; G. D. Lock20012001, vol.123, no.2
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