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35篇 您的检索式：作者名="TASLIM M E"

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	题名	作者	年代	出处	被引量
1	An experimental study of impingement on roughened airfoil leading edge walls with film holes显示文摘	Taslim M E Pan Y	2001	ASME Journal2001，123，：	1
2	Experimental and numerical investigations of impingement on a rib-roughened leading edge wall 显示文摘	Taslim M E Bakhtari K Liu H	2003	ASME Journal2003，125，：	1
3	Experimental and numerical im- pingement heat transfer in an airfoil leading-edge cooling channel with cross flow 显示文摘	Taslim M E Bethka D	2009	Journal of Turbomachinery2009，131，01：	1
4	An experimental investigation of film cooling effectiveness for slots of various exit geometries显示文摘	Taslim M E Spring S D Mehlmann B P		AIAA-90:2266 22730，90，22：	1
5	Experimental and numerical im- pingement heat transfer in an airfoil leading-edge cooling channel with cross flow显示文摘	Taslim M E Bethka D	2009	ASME Journal of Turbomach- inery2009，131，01：	1
6	Experimental and numerical study of impingement on an airfoil leading edge with and without showerhead and gill film holes显示文摘	Taslim M E Khanicheh A	2006	Journal of Turbomachinery2006，128，2：	1
7	An experimental evaluation of advanced leading edge impingement cooling concepts显示文摘	Taslim M E Setayeshgar L Spring S D	2001	Journal of Turbomachinery2001，123，：	1
8	Experimental and numerical impingement heat transfer in an airfoil leadlng-edge cooling channel with cross-flow显示文摘	Taslim M E Bethka D	2009	Journal of Turbomachinery2009，131，1：	1
9	An experimental study of impingement on roughened airfoil leading-edge walls with film holes 显示文摘	Taslim M E Pan Y Spring S D	2001	Journal of Transactions2001，123，：	1
10	Measurements of heat transfer coefficients and friction factors in passages ribroughened on all walls显示文摘	Taslim M E Li T Spring S D	1998	ASME Journal of Turbomachinery1998，120，2：	1
11	Experimental and numerical study of impingement on an airfoil leading edge with and without showerhead and gill film holes显示文摘	Taslim M E Khanicheh A	2006	Journal of Transactions2006，128，：	1
12	An experimental investigation of film cooling effectiveness for slots of various exit geometries显示文摘	Taslim M E Spring S D Mehlmann B P	1992	Journal of Thermophysics and Heat Transfer1992，6，2：	1
13	An Experimental Evaluation of Advanced Leading Edge Impingement Cooling Concepts显示文摘	TASLIM M E SETAYESHGAR L SPRING S D	2001	ASME Journal of Turbomachinery2001，123，1：	1
14	An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls with Film Holes显示文摘	TASLIM M E PAN Y SPRING S D	2001	ASME Journal of Turbomachinery2001，123，4：	1
15	Experimental and Numerical Investigation of Impingement on a Rib-Roughened Leading-Edge Wall显示文摘	TASLIM M E BAKHTARI K LIU H	2003	ASME Journal of Turbomachinery2003，125，4：	1
16	Experimental and Numerical Study of Impingement on an Airfoil Leading Edge With and Without Showerhead and Gill Film Holes显示文摘	TASLIM M E KHANICHEH A	2006	ASME Journal of Turbomachinery2006，128，2：	1
17	Experimental and Numerical Impingement Heat Transfer in an Airfoil Leading-Edge Cooling Channel With Cross-Flow显示文摘	TASLIM M E BETHKA D	2009	ASME Journal of Turbomachinery2009，131，01：	1
18	Experimental and Numerical Cross-Over Jet Impingement in an Airfoil Trailing-Edge Cooling Channel显示文摘	TASLIM M E NONGSAENG A	2011	ASME Journal of Turbomachinery2011，133，04：	1
19	An experimental evaluation advanced leading edge impingement cooling concepts显示文摘	Taslim M E Setayeshgar L Spring S D	2001	ASME Journal of Turbomachinery2001，123，1：	1
20	An experimental study of impingement on roughened airfoil leading edge walls with film holes显示文摘	Taslim M E Pan Y Spring S D	2001	Journal of Turbomachinery2001，123，10：	1

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