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20篇 您的检索式：作者名="Schobeiri"

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	题名	作者	年代	出处	被引量
1	Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model 显示文摘	SCHOBEIRI M T CHAKKA P	2002	International Journal of Heat and Mass Transfer2002，45，：	1
2	On the Physics of Flow Separation along a Low Pressure Turbine Blade Un- der Unsteady Flow Conditions显示文摘	Schobeiri M T Ozttirk B Ashpis D E	2005	Journal of Fluids Engi- neering2005，127，：	1
3	Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint 显示文摘	Ahn J Schobeiri M T Han J C	2006	Journal of Heat Transfer2006，128，：	1
4	GETRAN:A Generic,Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aro-and Power Generaion Gas Turbine Engines显示文摘	Schobeiri M T Attia M Lippke C	1994	Journal of Engineering for Gas Turbines and Power July1994，116，3：	1
5	Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint显示文摘	Ahn J Schobeiri M T Han J C	2006	Journal of Heat Transfer2006，128，：	1
6	Nonlinear dynamic simulation of single and multispool core engine, part I: computational method显示文摘	Schobeiri M T Atria M Lippke C	1994	AIAA Journal of Propulsion and Power1994，10，6：	1
7	Active control of compressor in stability and surge by stator blades adjustment显示文摘	Schobeiri M T Attia M	2003	Journal of Propulsion and Power2003，19，2：	1
8	GETRAN: a generic,modularly structured computer code for simulation of dynamic behavior of aero and power generation gas turbine engines显示文摘	Schobeiri M T ARia M Lippke C	1994	ASME Journal of Engineering for Gas Turbine and Power1994，116，：	1
9	On the Physics of Flow Separation Along a Low Pressure Turbine Blade Under Unsteady Flow Conditions 显示文摘	Schobeiri M T ()ztfirk B Ashpis D E	2005	ASME Journal of Fluids Engineering2005，127，50：	1
10	M T Turbine Blade Cooling Simulation in the Gas Turbine Engine Simulation Code Getran 显示文摘	Greendyke R B Schobeiri	2003	41st Aerospace Science Meeting and Exhibit2003，1214，：	1
11	Experimental Study of the Ef- fect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Reattaehment Along the Surface of a Low Pressure Turbine Blade显示文摘	Schobeiri M T 0zttirk B	2004	ASME Jour- nal of Turbomachinery2004，126，4：	1
12	Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Intermit- tency Behavior along the Suction Surface of a Low Pres- sure Turbine Blade 显示文摘	Schobeiri M T Oztirk B David E	2007	ASME Journal of Turbomachin- ery2007，129，1：	1
13	Active control of compressor in-stability and surge by stator blades adjustment显示文摘	Schobeiri M T Attia M	2003	Journalof Propulsion and Power2003，19，2：	1
14	Five-hole pressure probe analysis technique显示文摘	Morrison G Schobeiri M Pappu K	1998	Flow Measurement and In strumentation1998，9，：	1
15	Row-by-row off-design performance calculation method for turbines显示文摘	Schobeiri T Abouelkheir M	1992	Journal of Propulsion and Power1992，8，：	1
16	Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes 显示文摘	Ahn J Schobeiri M T Han J C	2007	International Journal of Heat and Mass Transfer2007，50，：	1
17	Five-Hole Pressure Probe Analysis Technique显示文摘	Morrison G L Schobeiri M T Pappu K R		0，，03：	1
18	Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint 显示文摘	Ahn J Schobeiri M T Hart J Q	2006	Journal of Heat Transfer2006，128，：	1
19	Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint显示文摘	Ahn J Schobeiri M T Han J C	2006	Journal of Heat Transfer2006，128，9：	1
20	Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes显示文摘	Ahn J Schobeiri M T Han J C	2007	International Journal of Heat and Mass Transfer2007，50，12：	1

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