PATENTS

Rotating Diesel Particulate Trap, US patent # 5,013,340, May 7, 1991

Enhanced Cooling Apparatus for Gas Turbine engine Airfoils, US patent # 5,472,316, December 5, 1995

Turbine Airfoil and Methods for Airfoil Cooling, US patent # 6,132,169 , October 17, 2000

Crossover Cooled Airfoil Trailing Edge, US patent # 6,607,356, August 19, 2003

Castellated Turbine Airfoil, US patent # 6,890,153, May 10, 2005

Non-Rotating Wind Energy Generator, US patent # 9,222,465, 2016

Device and Method for Chemical Analysis, Awarded, 2016

Orthopedic Device for Use with an Orthopedic Cast, Patent Application # US 2014/0330185 A1, Pending

BOOK CHAPTERS

Heat Transfer in Gas Turbines, WIT Press, ISBN 1-85312-666-7, 2001, B. Sunden and M. Faghri Editors, Chapter 8 : “Experimental Heat Transfer in Stationary Rib-Roughened Rectangular Channels”, pp. 291-405.

Heat Transfer in Gas Turbines, WIT Press, ISBN 1-85312-666-7, 2001, B. Sunden and M. Faghri Editors, Chapter 9 : “Experimental Heat Transfer in Roughened Leading- and Trailing-Edge and in Spanwise Rotating Channels”, pp. 407-520.

JOURNAL PUBLICATIONS

Taslim, M.E., Kinney, R.B., and Paolino, M.A., 1984, “Analysis of Two-Dimensional Viscous Flow Over an Elliptic Body in Unsteady Motion,” AIAA Journal, Vol. 22, No. 5, pp. 586-594.

Taslim, M.E. and Narusawa, U., 1986, “Binary Fluid Convection and Double Diffusive Convection in a Porous Medium,” J. Heat Transfer, Vol. 108, p. 221.

Pillatsis, G., Taslim, M.E. and Narusawa, U., 1987,”Thermal Instability of a Fluid-Saturated Porous Medium Bounded by Thin Fluid Layers,” Journal of Heat Transfer, Vol. 109, pp. 677-682.

Nayeb-Hashemi, H. and Taslim, M.E., 1987,”Effects of the Transient Mode II on the Steady State Crack Growth in Mode I”, J. Engr. Frac. Mech., Vol. 26, pp. 789-807.

Kinney, R.B., Taslim, M.E. and Hung, S.C., 1988, “A Hybrid Computational Approach to Multi-Body Viscous-Flow Problems: Application to Large-Eddy Breakup in a Boundary Layer,” J. Computational Physics, Vol. 77, No. 2, pp. 378-404.

Taslim, M.E. and Narusawa, U., 1989, ”Thermal Stability of a Horizontally Superposed Porous and Fluid Layers,” J. Heat Transfer, Vol. 111, No. 2, pp. 357-362.

Taslim, M.E., Rahman,A., and Spring, S.D., 1991, “An Experimental Investigation of the Heat Transfer Coefficients in a Spanwise Rotating Channel with Two Opposite Rib-Roughened Walls,” J. Turbomachinery, Vol. 113, pp. 75-82.

Taslim, M.E., Bondi, L.A. and Kercher, D.M., 1991,”An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened 45 Degree Criss-Cross Ribs on Two Opposite Walls,” J. Turbomachinery, Vol. 113, pp. 346-353.

Taslim, M.E., Spring, S.D., and B.P Mehlman, 1992,”An Experimental Investigation of Film Cooling Effectiveness for Slots of Various Exit Geometries,” J. Thermophysics Heat Transfer, Vol. 6, No. 2, pp. 302-307.

Bazydola, S.M. and Taslim, M.E., 1993, “An Experimental Investigation of a Staggered Array of Heatsinks in the Hydrodynamic and Thermal Entrance of a Duct,” J. Electronic Packaging, Vol. 115, No. 1, pp. 106-111.

El-Husayni, H., Taslim, M.E., and Kercher, D.M., 1994,”Experimental Heat Transfer Investigation of Stationary and Orthogonally Rotating Asymmetric and Symmetric Heated Smooth and Turbulated Channels,” J. Turbomachinery, Vol. 116, No. 1, pp. 124-132.

Taslim, M.E. and Spring, S.D., 1994,”Effects Turbulator Profile and Spacing Have on Heat Transfer and Friction in a Channel,” J. Thermophysics Heat Transfer, Vol. 8, No. 3, pp. 555-562.

Taslim, M.E., Li, T. and Spring, S.D., 1995,” Experimental Study of the Effects of Bleed Holes on Heat Transfer and Pressure Drop in Trapezoidal Passages with Tapered Turbulators,” J. Turbomachinery, Vol. 117, No. 2, pp. 281-289.

Taslim, M.E., Li, T. and Kercher, D.M., 1996, “Experimental Heat Transfer and Friction in Channels Roughened with Angled, V-Shape and Discrete Ribs on Two Opposite Walls,” J. Turbomachinery, Vol. 118, pp. 20-28.

Taslim, M.E. and Wadsworth, C.A., 1997, “An Experimental Investigation of the Rib Surface-Averaged Heat Transfer Coefficient in a Rib-Roughened Square Channel,” J. Turbomachinery, Vol. 119, pp. 381-389.

Taslim, M.E., Li, T. and Spring, S.D., 1997, “Measurement of Heat Transfer Coefficients and Friction Factors in Rib-Roughened Channels Simulating Leading-Edge Cavities of a Modern Turbine Blade,” J. Turbomachinery, Vol. 119, pp. 411-419.

Korotky, G.J. and Taslim, M.E., “Rib Heat Transfer Coefficient Measurements in a Rib-Roughened Square Passage,” J. Turbomachinery, Vol. 120, No. 2, pp. 376-385.

Taslim, M.E., Li, T. and Spring, S.D., Measurement of Heat Transfer Coefficients and Friction Factors in Passages Rib-Roughened on All Walls,” J. Turbomachinery, Vol. 120, pp. 564-570.

Taslim, M.E., and A. Lengkong, 1998, “45o Staggered Rib Heat Transfer Coefficient Measurements in a Square Channel,” J. Turbomachinery, Vol. 120, pp. 571-580.

Taslim, M.E., and G.J. Korotky, 1998, “Low-Aspect-Ratio Rib Heat Transfer Coefficient Measurements in a Square Channel,” J. Turbomachinery, Vol. 120, pp. 831-838.

Taslim, M.E., and A. Lengkong, 1999, “45o Round-Corner Rib Heat Transfer Coefficient Measurements in a Square Channel,” J. Turbomachinery, Vol. 121, pp. 1-9.

Taslim, M.E., , L. Setayeshgar, and Spring, S.D., 2001, “ An Experimental Evaluation of Advanced Leading-Edge Impingement Cooling Concepts,” J. Turbomachinery, Vol. 123, No. 2, pp. 147-153.

Taslim, M.E., Pan, Y. and Spring, S.D., 2001, “An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls with Film Holes” J. Turbomachinery, Vol. 123, No. 4, pp. 766-773.

Taslim, M.E., Bakhtari, K., and H. Liu, 2003, “Experimental and Numerical Investigation of Impingement on a Rib-Roughened Leading-Edge Wall,” J. Turbomachinery, Vol. 125, pp. 682-691.

Taslim, M.E. and Ugarte, S., 2004, “Discharge Coefficient Measurements for Flow Through Compound-Angle Conical Holes with Crossflow,” Int. J. Rotating Machinery, Vol. 10, No. 2, pp. 145-153.

Talim, M.E. and Liu, H., 2005, “A Combined Numerical and Experimental Study of Heat Transfer in a Roughened Square Channel with 45o Ribs,” Int. J. Rotating Machinery, Vol. 2005, No. 1 , pp. 60-66 .

Taslim, M.E. and Khanicheh, A., 2005, “Film Effectiveness Downstream of a Row of Compound Angle Film Holes”, J. Heat Transfer, Vol. 127, No. 4, pp. 434-440.

M.E Taslim, 2005, “Rib Fin Effects on the Overall Equivalent Heat Transfer Coefficient in a Rib-Roughened Cooling Channel,” Int. J. Heat Exchangers, Vol. VI, No. 2, pp. 135-151.

Taslim, M.E. and Khanicheh, A., 2006, “Experimental and Numerical Study of Impingement on an Airfoil Leading-Edge with and Without Showerhead and Gill Film Holes,” J. Turbomachinery, Vol. 128, No. 2, pp. 310-320.

Cakan, M and Taslim, M.E., 2007, “Experimental and Numerical Study of Mass/Heat Transfer on an Airfoil Trailing-Edge Slot and Lands,” J. Turbomachinery, Vol. 129, No. 2, pp. 281-293.

Taslim, M.E. and Nezym, V., “A New Statistical-Based Correlation for the Rib Fin Effects on the Overall Heat Transfer Coefficient in a Rib-Roughened Cooling Channel,” Int. J. Rotating Machinery, Vol. 2007, Article ID 68684.

James V. Green, J.V, Kniazeva, T., Abedi, M., Sokhey, D., Taslim, M.E., and Murthy, S., 2008, ‘’ Effect of channel geometry on cell adhesion in micro-fluidic devices’’ Lab on a Chip J., Royal Society of Chemistry, pp. 1-10.

Taslim, M.E. and Bethka, D., 2009, “Experimental and Numerical Impingement Heat Transfer in an Airfoil Leading-Edge Cooling Channel With Cross-flow,” J. Turbomachinery, Vol. 131 , No. 1, pp. 011021-1-011021-7.

Taslim, M.E., Khanicheh, A. and Spring, S.D., 2009 “A Numerical Study of Sand Separation Applicable to Engine Inlet Particle Separator Systems”, J. American Helicopter Society, Vol. 54, No. 4, pp. 2001-2010.

Taslim, M.E., and Spring, S.D., 2010 “A Numerical Study of Sand Particle Distribution, Density and Sand Shape Effects on the Scavenge Efficiency of Engine Inlet Particle Separator Systems”, J. American Helicopter Society, Vol. 54, No. 5, pp. 2201-2211.

Taslim, M.E. and Abdelrassoul, A., 2010, “An Experimental and Numerical Investigation of Impingement Heat Transfer in Airfoils Leading-Edge Cooling Channel,” J. of Heat Transfer Research, issue 8, Vol. 41, pp. 100-108 .

Taslim, M.E. and Nongsaeng, A., 2011 ,“ Experimental and Numerical Cross-Over Jet Impingement in an Airfoil Trailing-Edge Cooling Channel”, J. Turbomachinery, Vol. 133, No. 4, pp. 041009-1-10.

Adebiyi, A.A., Taslim, M.E. and Crawford, K.D., 2011 ,“The Use of Computational Fluid Dynamic Models for the Optimization of Cell Seeding Processes”, J. Biomaterials , doi:10.1016/j.biomaterials.2011.08.028

Elebiary, K. and Taslim, M.E., 2013,“ Experimental/Numerical Cross-Over Jet Impingement in an Airfoil Leading-Edge Cooling Channel”, J. Turbomachinery , Vol. 135, No. 1, pp. 011037-1-12.

Taslim, M.E. and Fong, M.K.H., 2013 ,“ Experimental and Numerical Cross-Over Jet Impingement in a Rib-Roughened Airfoil Trailing-Edge Cooling Channel”, J. Turbomachinery, Vol. 135, No. 5, pp. 051014-1-10.

Taslim, M.E. and Huang, X., 2014,“ Experimental/Numerical Investigation on the Effects of Trailing-Edge Cooling Hole Blockage on Heat Transfer in a Trailing-Edge Cooling Channel”, J. Gas Turbine Power, Vol. 136, No. 5, pp. 082603-1-15.

Taslim, M.E. and Halabi, J.S.., 2014,“ Experimental/Numerical Investigation on the Effects of Trailing-Edge Cooling Hole Blockage on Heat Transfer in a Trailing-Edge Cooling Channel”, Int. J. Rotating Machinery, Volume 2014, Article ID 710450, http://dx.doi.org/10.1155/2014/710450

Taslim, M.E. and Xue, F., 2017, “Crossover Jet Impingement in a Rib-Roughened Trailing-Edge Cooling Channel”, J. Turbomachinery (in press).

Adebiyi, A. and Taslim, M.E. 2017, “Evaluation of Different Pseudo-potential Based Multicomponent Multiphase Lattice Boltzmann Wetting models for a Droplet-Based System’, Int. J. of Multiphase Flow (under review).

REFEREED CONFERENCE PROCEEDINGS

M.E. Taslim and U. Narusawa, 1984, “Cross Diffusion Instability and Double-Diffusive Instability in a Fluid-Saturated Porous Medium,” 22nd National Heat Transfer Conference, Niagara Falls, New York.

M.E. Taslim, U. Narusawa, and G. Pillatsis, 1985, “Convective Stability of a Fluid-Saturated Porous Layer Sandwiched Between Two Fluid Layers,” 23rd National Heat Transfer Conference, Denver, Colorado.

H. Nayeb-Hashemi, M.E. Taslim, J. Zotos and M.D. Cohen, 1985, “Effect of Mode II Overload on Subsequent Mode I Crack Growth,” Proc. Int. Conf. And Exposition on Fatigue, Corrosion Cracking, Fracture Mechanics and Failure Analysis, pp. 387-398, Salt Lake City, Utah.

G. Pillatsis, G. Derjani, M.E. Taslim and U. Narusawa, 1986,”Effects of Boundary Conditions on Thermal Instability of Superposed Porous and Fluid Layers,”ASME Pub. No. HTD-Vol. 56, pp. 55-60, 4th AIAA/ASME Thermophysics and Heat Transfer Conference, Boston, Massachusetts.

G. Derjani, M.E Taslim and U. Narusawa, 1986, “Convective Stability of a Combined System of a Porous and a Fluid Layer,”ASME Winter Annual Meeting, Pub. No. HTD-Vol. 63, pp. 83-89, Anaheim, California.

M.E. Taslim and U. Narusawa, 1987, “Convective Stability of a Horizontal Fluid Layer Bounded by Two Porous Layer,” Proceedings of the ASME-JSME Thermal Engineering Joint Conference, Vol. 2, pp. 387-393, Honolulu, Hawaii.

M.E. Taslim and S.D. Spring, 1987, “Friction Factors and Heat Transfer Coefficients in Turbulated Cooling Passages of Different Aspect Ratios, Part I: Experimental Results,” AIAA/SAE/ASME/ASEE 23rd Joint Propulsion Conference, San Diego, California, Paper no. AIAA-87-2009.

M.E. Taslim and S.D. Spring, 1988, “An Experimental Investigation of Heat Transfer Coefficients and Friction Factors in Passages of Different Aspect Ratios Roughened with 45o Turbulators,” ASME National Heat Transfer Conference, Houston, Texas.

M.E. Taslim and S.D. Spring, 1988, “An Experimental Investigation of Heat Transfer Coefficients and Friction Factors in Passages of Different Aspect Ratios Roughened with 90o Staggered Turbulators,” AIAA/ASEE/ASME/SAE 24th Joint Propulsion Conference and Exhibit, Boston, MA.

M.E. Taslim, A. Rahman and S.D. Spring, 1989, “An Experimental Investigation of Heat Transfer Coefficients in a Spanwise Rotating Channel With Two Opposite Rib-Roughened Walls,” ASME Paper No. 89-GT-150, 34th ASME International Gas Turbine Conference, Toronto, Canada.

M.E. Taslim, A. Rahman, 1989, “An Experimental Investigation of the Heat Transfer Enhancement in the Cooling Passages of Modern Gas Turbine Blades,”International Symposium on Thermodynamic Analysis and Improvement of Energy Systems, Beijing, China.

M.E. Taslim, U. Narusawa and H. Rafiotis, 1989, “A Thermocapillary Flow Induced by a Surface Heat Flux Variation,” 26th ASME National Heat Transfer Conference, Pub. No. HTD-Vol. 113, pp. 85-93, Philadelphia, PA.

M.E. Taslim, C. Chrysafis and D.M. Kercher, 1989, “An Experimental Study of Heat Transfer in a Spanwise Rotating Channel Turbulated with 45 Degree Criss-Cross Ribs,” Proc. of ASME Winter Annual Meeting, San Francisco, CA.

M.E. Taslim, L.A. Bondi and D.M. Kercher, 1990, “An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened with 45o Criss-Cross Ribs on Two Opposite Walls,” 35th ASME International Gas Turbine Conference, Brussels, Belgium.

Y.A. Levendis, T. Panagiotou and M.E. Taslim, 1990, “Development of a Self-Cleaning Particle Trap for Diesel Engine Particulate Control,” SAE International Congress and Exhibition, Detroit, MI.

M.E. Taslim, 1990, “Application of Liquid Crystals in Heat Transfer Coefficient Measurement,” Proc. of ELECTRO/90 Electronic Convention, Boston, MA.

M.E. Taslim, S.D. Spring, and B.P Mehlman, 1990, “An Experimental Investigation of Film Cooling Effectiveness for Slots of Various Exit Geometries,” 26th Joint AIAA/SAE/ASME/ASEE Propulsion Conference, Orlando, FL, Paper # AIAA-90-2266.

M.E. Taslim and S.D. Spring, 1991, “An Experimental Investigation into the Effects Turbulator Profile and Spacing Have on Heat Transfer Coefficients and Friction Factors in Small Cooled Turbine Airfoils,” 27th AIAA/SAE/ASME Joint Propulsion Conference, Sacramento, CA, Paper # AIAA-91-2033.

S.M. Bazydola and M.E. Taslim, 1992, “An Experimental Investigation of a Staggered Array of Heatsinks in the Hydrodynamic and Thermal Entrance of a Duct,” ASME/IEEE/ISHM/NIST Third Intersociety Conference on Thermal Phenomena in Electronic Systems, Austin, TX.

H. El-Husayni, M.E. Taslim, and D.M. Kercher, 1992, “Experimental Heat Transfer Investigation of Stationary and Orthogonally Rotating Asymmetric and Symmetric Heated Smooth and Turbulated Channels,” 37th ASME International Gas Turbine Conference, Colone, Germany, June 1992.

M.E. Taslim, T. Li and S.D. Spring, 1993, “Experimental Study of the Effects of Bleed Holes on Heat Transfer and Pressure Drop in Trapezoidal Passages with Tapered Turbulators,” 38th ASME International Gas Turbine Conference, Cincinnati, Ohio, June 1993.

M.E. Taslim, T. Li and D.M. Kercher, 1994, “Experimental Investigation of Heat Transfer and Friction in a Channel Roughened with $45^circ$, $90^circ$, V-Shape and Broken Angled Ribs on Two Opposite Walls,” 39th ASME International Gas Turbine Conference, Hague, Netherlands, June 1994.

M.E. Taslim and C.M. Wadsworth, 1994, “An Experimental Investigation of the Rib Surface-Averaged Heat Transfer coefficient in a Rib-Roughened Square Passage,” 39th ASME International Gas Turbine Conference, Hague, Netherlands, June 1994.

M.E. Taslim, T. Li and S.D. Spring, 1994, “Measurement of Heat Transfer Coefficients and Friction Factors in Rib-Roughened Channels Simulating Leading-Edge Cavities of a Modern Turbine Blade,” 40th ASME International Gas Turbine Conference, Houston, TX, June 1995.

G.J. Korotky and M.E. Taslim, 1995, “Measurement of Surface-Averaged Heat Transfer Coefficient in a Square Passage Roughened with Round-Corner Ribs,” The Third Asian Pacific International Symposium on Combustion and Energy Utilization, Hong Kong.

M.E. Taslim, T. Li and S.D. Spring, 1996, “Measurements of Heat Transfer Coefficient and Friction Factors in Passages Rib-Roughened on All Walls,” 41st. International Gas Turbine and Aeroengine Congress and Exposition, Birmingham, England.

G.J. Korotky, M.E Taslim, 1996, “Rib Heat Transfer Coefficient Measurements in a Rib-Roughened Square Passage,” 41st. International Gas Turbine and Aeroengine Congress and Exposition, Birmingham, England, Paper # 96-GT-356.

M.E. Taslim and A. Lengkong, 1996, “45o Rib Heat Transfer Coefficient Measurements in a Square Channel,” ASME Turbo Asia '96 Conference, Jakarta, Indonesia, Paper # 96-TA-9.

M.E Taslim, G.J. Korotky, 1997, “Low Aspect Ratio Rib Heat Transfer Coefficient Measurements in a Square Channel,” 42nd. asme International Gas Turbine and Aeroengine Congress, Exposition and Users Symposium, Orlando, Florida, Paper # 97-GT-388.

M.E. Taslim and A. Lengkong, 1998, “45o Round-Corner Rib Heat Transfer Coefficient Measurements in a Square Channel,” 43rd. ASME International Gas Turbine and Aeroengine Congress, Exposition and Users Symposium, Stockholm, Sweden, Paper # 98-GT-176.

M.E. Taslim, T. Li, and S.D. Spring, 1998, “Measurements of Heat Transfer Coefficient in Rib-Roughened Trailing-Edge Cavities with Crossover Jets,” 43rd. ASME International Gas Turbine and Aeroengine Congress, Exposition and Users Symposium, Stockholm, Sweden, Paper # 98-GT-435.

M.E Taslim, S. Ugarte, 2000, “Discharge Coefficient Measurements for Flow Through Compound-Angle Conical Holes with Crossflow,” The 8th. International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii.

M.E Taslim, L. Setayeshgar, 2000, “An Experimental Evaluation of Advanced Leading-Edge Impingement Cooling Concepts,” 45th. ASME International Gas Turbine and Aeroengine Congress, Exposition and Users Symposium, Munich, Germany, Paper # 2000-GT-0222.

M.E. Taslim, and Setayeshgar, L.,2001, “Experimental Leading-Edge Impingement Cooling Through Racetrack Crossover Holes”, The 46th ASME International Gas Turbine and Aeroengine Conference and Exposition, New Orleans, Louisiana, .

M.E. Taslim, Y. Pan, and S.D. Spring, 2001, “An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls with Film Holes”, The 46th ASME International Gas Turbine and Aeroengine Conference and Exposition, New Orleans, Louisiana.

M.E Taslim, 2002, “Rib Fin Effects on the Overall Equivalent Heat Transfer Coefficient in a Rib-Roughened Cooling Channel of a Turbine Airfoil,” The 9th. International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii.

M.E. Taslim, Y. Pan, and K. Bakhtari, 2002, “Experimental Racetrack Shaped Jet Impingement on a Roughened Leading-Edge Wall with Film Holes,” The 47th ASME International Gas Turbine and Aeroengine Conference and Exposition, Amsterdam, Paper # GT-2002-30477.

Taslim, M.E., Bakhtari, K., and H. Liu, 2003, “Experimental and Numerical Investigation of Impingement on a Rib-Roughened Leading-Edge Wall, ” The 48th ASME International Gas Turbine & Aeroengine Conference & Exposition, Atlanta, Georgia, Paper # GT-2003-38118.

Khanicheh, A. and Taslim, M.E., 2003, “Experimental and Numerical Film Effectiveness Downstream a Row of Compound Angle Film Holes”, IMECE, Washington, D.C., IMECE2003-41414.

Taslim, M.E. and Liu, H., 2004, “A Combined Numerical and Experimental Study of Heat Transfer in a Roughened Square Channel with 45o Ribs,” The 10th. International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, Paper # ISROMAC10-2004-108

Taslim, M.E., Khanicheh, A., Spring, S.D., and W. Oliver, 2004, “A Numerical Study of Sand Separation Applicable to Engine Inlet Particle Separator Systems”, American Helicopter Society Conference, June 8-10, 2004, Baltimore, Maryland.

Taslim, M.E. and Khanicheh, A., 2005, “Experimental and Numerical Study of Impingement on an Airfoil Leading-Edge with and Without Showerhead and Gill Film Holes,” The 49th ASME International Gas Turbine and Aeroengine Conference and Exposition, Reno-Taho, Nevada, USA, Paper # GT-2005-68037.

Taslim, M.E. and Nezym, V., 2006, “A New Statistical-Based Correlation for the Rib Fin Effects on the Overall Heat Transfer Coefficient in a Rib-Roughened Cooling Channel,” The 11th. International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, Paper # ISROMAC11-2006-212.

Cakan, M and Taslim, M.E., 2006, “Experimental and Numerical Study of Mass/Heat Transfer on an Airfoil Trailing-Edge Slot and Lands,” The 50th ASME International Gas Turbine and Aeroengine Conference and Exposition, Barcelona, Spain, Paper # GT-2006-91202.

Taslim, M.E. and Bethka, D., 2007, “Experimental and Numerical Impingement Heat Transfer in an Airfoil Leading-Edge Cooling Channel With Cross-flow,” The 51st ASME International Gas Turbine and Aeroengine Conference and Exposition, Montreal, Canada, Paper # GT-2007-28212.

Taslim, M.E. and Nicolas, G., 2008, “An Experimental and Numerical Investigation of Jet Impingement on Ribs in an Airfoil Trailing-Edge Cooling Channel,” The 12th. International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, Paper # ISROMAC12-2008-20238.

Shapiro, J.D. and Taslim, M.E., 2008 ,“Experimental Heat Transfer and Discharge Coefficients for Single Confined Jet Impingement Normal to a Surface at Close Distances”, The 52nd ASME International Gas Turbine and Aeroengine Conference and Exposition, Montreal, Canada, Paper # GT-2008-50080.

Taslim, M.E. and Abdelrassoul, A., 2009, “An Experimental and Numerical Investigation of Impingement Heat Transfer in Airfoils Leading-Edge Cooling Channel,” Int. Symp. on Heat Transfer in Gas Turbine Systems, 9-14 August, 2009, Antalya, Turkey.

Taslim, M.E. and Nongsaeng, A., 2010 ,“ Experimental and Numerical Cross-Over Jet Impingement in an Airfoil Trailing-Edge Cooling Channel”, ASME Turbo Expo 2010, Glasgow, UK, June 14-18, 2010, Paper # GT2010-23521.

Taslim, M.E. and Fong, M.K.H., 2011 ,“ Experimental and Numerical Cross-Over Jet Impingement in a Rib-Roughened Airfoil Trailing-Edge Cooling Channel”, ASME Turbo Expo 2011, Vancouver, CA, June 14-18, 2011, Paper # GT2011- 45995.

Elebiary, K. and Taslim, M.E., 2011,“ Experimental/Numerical Cross-Over Jet Impingement in an Airfoil Leading-Edge Cooling Channel”, ASME Turbo Expo 2011, Vancouver, CA, June 14-18, 2011, Paper # GT2011- 46004.

Smyser, B.M., Kowalski, G.J. and Taslim, M.E. ,”Small Business Sponsored Projects: Factors for Success”, 2012 Capstone Design Conference, May 30 - June 1, 2012, Champaign-Urbana, Illinois, Paper ID:17.

Taslim, M.E. and N. Rosso, 2012,“ Experimental/Numerical Study of Multiple Rows of Confined Jet Impingement Normal to a Surface at Close Distances”, ASME Turbo Expo 2012, Copenhagen, Denmark, June 11-15, 2012, Paper # GT2012- 68634.

Taslim, M.E. and Huang, X., 2013,“ Experimental/Numerical Investigation on the Effects of Trailing-Edge Cooling Hole Blockage on Heat Transfer in a Trailing-Edge Cooling Channel”, ASME Turbo Expo 2013, San Antonio, Texas, USA, June 3-7, 2013, Paper # GT2013-95859.

Taslim, M.E. and Halabi, J.S.., 2014,“ Experimental/Numerical Investigation on the Effects of Trailing-Edge Cooling Hole Blockage on Heat Transfer in a Trailing-Edge Cooling Channel”, ASME Turbo Expo 2014, Dusseldorf, Germany, June 16-19, 2014, Paper # GT2014-27130.

Taslim, M.E. and Xue, F., 2015, “Experimental/Numerical Investigation of Cross-Over Jet Impingement in a Rib-Roughened Trailing-Edge Cooling Channel”, Turbo-Expo Turbomachinery Technical Conference & Exposition, Seoul, South Korea, June 13-17,2016, Paper # GT2016-56139.