RECENT LECTURES, INCLUDING INVITED LECTURES

  1. Recent Developments in Field Flow Fractionation and Continuous SPLITT Fractionation, FFF (Field Flow Fractionation) Research Center, Chemistry Department, University of Utah, Salt Lake City, Utah, USA, October 21, 1994.
  2. Recent Developments in Field Flow Fractionation and Continuous SPLITT Fractionation, Dow Chemical Corporation, Midland, Michigan, USA, October 25, 1994.
  3. Recent Gas Turbine Heat Transfer Research at the University of Utah, Solar Turbines Inc., San Diego, California, USA, April 7, 1995
  4. Flow and Heat Transfer in a Curved Channel Including Development and Characteristics of Dean Vortices, Nagoya Institute of Technology, Nagoya, Japan, July 11, 1995.
  5. Flow and Heat Transfer in a Curved Channel Including Development and Characteristics of Dean Vortices, Kyoto University, Kyoto, Japan, July 14, 1995.
  6. Effects of Bulk Flow Pulsations on Film Cooling, Mitsubishi Heavy Industries Ltd., Takasago Research and Development Center, Takasago, Japan, July 19, 1995.
  7. Effects of Bulk Flow Pulsations on Film Cooling, Kyushu University, Fukuoka, Japan, July 21, 1995.
  8. Study of Vortices in Turbulent Flow to Augment Surface Heat Transfer, Solar Turbines Inc., San Diego, California, USA, November 13, 1996.
  9. Heat Transfer in Curved and Straight Channels, Idaho State University, Pocatello, Idaho, USA, January 17, 1997.
  10. Gas Turbine Heat Transfer Research at the University of Utah, Department of Mechanical Engineering, Undergraduate Seminar, University of Utah, Salt Lake City, Utah, USA, March 4, 1997.
  11. Heat Transfer and Fluid Mechanics Research at the University of Utah Convective Heat Transfer Laboratory, Rocketdyne Corporation, Canoga Park, California, USA, July 17, 1998.
  12. Gas Turbine Heat Transfer Research at the University of Utah, Department of Mechanical Engineering, Undergraduate Seminar, University of Utah, Salt Lake City, Utah, USA, November 10, 1998.
  13. Swirl Chamber Heat Transfer and Flow Characteristics, General Electric Corporate Research and Development Center, Schenectady, New York, USA, August 5, 1999.
  14. Innovative Schemes for Convective Heat Transfer Augmentation, Darmstadt Technical University, Darmstadt, Germany, May 30, 2000.
  15. Effects of Roughness on the Development and Structure of Turbulent Boundary Layers, Department of Mechanical Engineering, Louisiana State University, Baton Rouge, Louisiana, USA, September 8, 2000.
  16. Transonic Aerodynamic Losses Due to Turbine Airfoil, Suction Surface Film Cooling, Department of Mechanical Engineering, Louisiana State University, Baton Rouge, Louisiana, USA, October 25, 2000.
  17. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Department of Mechanical Engineering, North Carolina State University, Raleigh, North Carolina, USA, November 28, 2000.
  18. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Department of Mechanical Engineering, University of Massachusetts, Amherst, Massachusetts, USA, March 12, 2001.
  19. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, National Science Foundation, Chemical and Transport Systems Division, Arlington, Virginia, USA, March 24, 2001.
  20. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Pratt & Whitney – Canada Corporation, Longueille, Quebec, Canada, September 7, 2001.
  21. The Influences and Effects of Different Physical Phenomena on Film Cooling, Pratt & Whitney – Canada Corporation, Longueille, Quebec, Canada, September 7, 2001.
  22. Dimpled Tube Development, Gas Technology Institute, Des Plaines, Illinois, USA, February 22, 2002.
  23. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Department of Mechanical Engineering, Ohio University, Athens, Ohio, USA, February 25, 2002.
  24. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Department of Mechanical Engineering, University of Akron, Akron, Ohio, USA, February 26, 2002.
  25. Heat Transfer and Flow Structure On and Above a Dimpled Surface in a Channel, Department of Mechanical Engineering, Kansas State University, Manhattan, Kansas, USA, October 24, 2002.
  26. Micropumps for Low-Volume Drug Delivery, Sorenson Medical Corp., Salt Lake City, Utah, USA, September 16, 2003.
  27. Electrochemical Actuation of Micropumps, and Micropumps for Low-Volume Drug Delivery, Ceramatec Advanced Materials and Electrochemical Technologies Corp., Salt Lake City, Utah, USA, November 11, 2003.
  28. Osmotic Dispense Pump, Foxboro-Invensys Corporation, Foxboro, Massachusetts, USA, December 15, 2004.
  29. Research Underway in the Convective Heat Transfer Laboratory at the University of Utah, Foxboro-Invensys Corporation, Foxboro, Massachusetts, USA, December 15, 2004.
  30. Osmotically-Driven Dispense Pump, ARUP Institute for Clinical and Experimental Pathology, Salt Lake City, Utah, USA, March 23, 2005.
  31. Heat Transfer and Flow Structure On and Above Dimpled Surfaces in Macro- and Micro-Scale Channels, Department of Mechanical and Industrial Engineering, University of Illinois at Chicago, Chicago, Illinois, USA, March 28, 2005.
  32. Vision Seminar: Future Directions in Macro-Fluid Mechanics, Micro-Fluid Mechanics, and Heat Transfer, Department of Mechanical and Industrial Engineering, University of Illinois at Chicago, Chicago, Illinois, USA, March 29, 2005.
  33. Miniature-Scale and Millimeter-Scale Rotating Shaft Pumps (RSP), Price Pump Company, Sonoma, California, USA, May 31, 2005.
  34. Research Projects – Convective Heat Transfer Laboratory – University of Utah, Intel Corporation – Visit and Discussions, Department of Mechanical Engineering, University of Utah, Salt Lake City, Utah, September 8, 2005.
  35. Convective Heat Transfer Laboratory – Future Directions in Macro-Fluid Mechanics, Micro-Fluidics, and Heat Transfer, Department of Mechanical Engineering, University of Utah, Salt Lake City, Utah, September 23, 2005.
  36. A Vision for Turbomachinery and Related Research in the Osney Laboratory, Department of Engineering Science, Oxford University, Oxfordshire, England, United Kingdom, October 28, 2005.
  37. Aero Losses, Heat Transfer, and Discharge Coefficients for Different Vane Trailing Edge Configurations, UTSR Peer Review Workshop III, Madren Conference Center and Inn, Clemson University, Clemson, South Carolina, October 19-21, 2005.
  38. Dimple Array Effects on Heat Transfer and Turbulent Flow Structure, Keynote Lecture, Fifth International Symposium on Turbulence, Heat, and Mass Transfer, Dubrovnik, Croatia, September 25-29, 2006.
  39. Oxford Rotor Group CFD – Oxford Aerodynamics and Heat Transfer UTC – Turbomachinery Laboratory (N. Atkins, G. Thomas, R. W. Ainsworth, P. M. Ligrani), Rolls-Royce CFD Annual Review, Rolls-Royce PLC, Morley, Derbyshire, England, United Kingdom, October 5-6, 2006.
  40. Future Research and Development Directions in Fluid Mechanics and Heat Transfer, QinetiQ PLC, Cody Technology Park, Farnborough, England, United Kingdom, November 13, 2006.
  41. Dimple Array Effects on Turbulent Heat Transfer and Flow Structure, Aeronautics Department, Prince Consort Road, Imperial College of Science, Technology, and Medicine, University of London, London, England, United Kingdom,, December 6, 2006.
  42. Turbomachinery Laboratory – Review of Laboratory Activities – Aerodynamics, Heat Transfer, and Turbomachinery Group, Presentation to Dr. Dr. Bauer and Dr. Schulz of ITS – Institut fuer Thermische Stroemungsmaschinen – Universitaet Karlsruhe, Thermo-Fluids Laboratory, Oxford University, Oxford, England, United Kingdon, January 8, 2007.
  43. Thermo-Fluids Laboratory–Aerodynamics, Heat Transfer, and Turbomachinery Group, Institut fuer Thermische Stroemungsmaschinen, Universitaet Karlsruhe, Germany, January 22, 2007.
  44. Turbine Vane Aerodynamic Losses With and Without Surface Roughness Augmentations, Fachgebiet Stromungslehre und Aerodynamik Technische Universitat, Technical University of Darmstadt, Darmstadt, Germany, January 29, 2007.
  45. Oxford Rotor Group CFD Work on Tip Flow and Heat Transfer, Rolls-Royce Annual Tip Cooling Forum, Rolls Royce PLC, Bristol, England, United Kingdom, February 6, 2007.
  46. Current State-of-the-Art Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Future Directions, Siemens Corporation, Ruston House, Lincoln, England, United Kingdom, April 24, 2007.
  47. Microfluidic Separation of Biological Nano-Particles (with Dr. Karl Morten), John Fell Fund Program, Oxford University, Oxford, England, United Kingdom, May 9, 2007.
  48. The Impetus for Nano-Technology and Micro-Science Research in the Department of Engineering Science at Oxford University (with Dr. Yiannis Ventikos), Engineering Program Visit, EPSRC-Engineering and Physical Sciences Research Council, Department of Engineering Science, Oxford University, Oxford, England, United Kingdom, June 11, 2007.
  49. Microfluidic Separation of Biological Nano-Particles (with Dr. Karl Morten), UCSF / IUIF / ISIS Innovation Funding Program, Oxford University, Oxford, England, United Kingdom, July 5, 2007.
  50. Microfluidic Separation of Biological Nano-Particles (with Dr. Karl Morten), Becton, Dickinson, and Company Visit, Department of Engineering Science, Begbroke Centre for Innovation and Enterprise, Oxford University, Oxford, England, United Kingdom, July 17, 2007.
  51. Current State-of-the-Art Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Future Directions, Rolls Royce PLC, Thermo-Fluids Laboratory, Department of Engineering Science, Oxford University, Oxford, England, United Kingdom, August 21, 2007.
  52. Oxford Rotor Group CFD Work (A. Wheeler, Q. Zhang, N. Atkins, G. Thomas, P. M. Ligrani, R. W. Ainsworth), Rolls-Royce CFD Annual Review, Rolls-Royce PLC, Morley, Derbyshire, United Kingdom, October 1-2, 2007.
  53. Effects of a Casing Step on the Over-Tip Aerothermodynamics of a Transonic HP Turbine Stage, Institute for Energy Technologies, Swiss Federal Institute of Technology, ETH Zurich, Switzerland, October 24, 2007.
  54. Smart Materials and Smart Structures for Aerodynamicists: Benefits, Challenges, Opportunities, Visions. Invited Lecture – Aerospace 2030 – The Role of Smart Materials, Begbroke Centre for Innovation and Enterprise, Department of Engineering Science, Oxford University, Oxford, England, United Kingdom, November 27, 2007.
  55. Technology Trends in the Gas Turbine Industry, Invited Keynote Paper – 4th International Conference on the Future of Gas Turbine Technology, European Turbine Network Conference, Brussels, Belgium, October 15, 2008.
  56. Suction-Side Gill-Region Film Cooling: Effects of Hole Shape and Orientation on Adiabatic Effectiveness, Heat Transfer Coefficient, and Aerodynamic Performance, Siemens Energy Inc., Muelheim an der Ruhr, Germany, November 19, 2008.
  57. Suction-Side Turbine Vane Film Cooling: Thermal and Aerodynamic Performance to Meet Energy and Environmental Challenges, Department of Mechanical and Aerospace Engineering, University of Notre Dame, Notre Dame, Indiana, December 15, 2008.
  58. Suction-Side Turbine Vane Film Cooling: Thermal and Aerodynamic Performance to Meet Energy and Environmental Challenges, Department of Mechanical Engineering, The Petroleum Institute, Abu Dhabi, United Arab Emerites, December 23, 2008.
  59. Current State-of-the-Art Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Future Directions, Heat Transfer Advance Technology Group, Siemens Energy Inc., Orlando, Florida, May 28, 2009 and June 18, 2009.
  60. A Vision for the Oliver L. Parks Endowed Chair and Director of Graduate Programs at Saint Louis University, Parks College of Engineering, Aviation and Technology, Saint Louis University, St. Louis, Missouri, USA, January 25, 2010.
  61. Flow and Heat Transfer on and Near a Transonic Turbine Blade Tip, Including Effects of a Varying Tip Gap, Department of Mechanical Engineering, Louisiana State University, Baton Rouge, Louisiana, USA, February 5, 2010.
  62. Flow and Heat Transfer on and Near a Transonic Turbine Blade Tip, Including Effects of a Varying Tip Gap, Department of Mechanical and Aerospace Engineering, Florida Institute of Technology, Melbourne, Florida, USA, February 9, 2010.
  63. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Department of Mechanical Engineering, University of Texas at Dallas, Dallas, Texas, USA, February 18, 2010.
  64. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, William Maxwell Reed Seminar, Department of Mechanical Engineering, University of Kentucky, Lexington, Kentucky, USA, March 23, 2010.
  65. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Department of Aerospace and Mechanical Engineering, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, September 9, 2010.
  66. Current State-of-the-Art Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Future Directions, Advanced Technology Turbine, Mechanical Center of Excellence, Honeywell Engine and Air Management, Honeywell Aerospace Division, Honeywell International Corp., Phoenix, Arizona, USA, September 24, 2010.
  67. Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Measurement Techniques, School of Mechanical and Automotive Engineering, Inje University, Gimhae, South Korea, October 4, 2010.
  68. Flow and Heat Transfer On and Near a Transonic Turbine Blade Tip, Including Effects of a Varying Tip Gap, School of Mechanical and Automotive Engineering, Inje University, Gimhae, South Korea, October 5, 2010.
  69. Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Measurement Techniques, Department of Mechanical Engineering, KAIST – Korea Advanced Institute of Science and Technology, Daejeon, South Korea, October 6, 2010.
  70. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, School of Mechanical and Aerospace Engineering, College of Engineering, SNU – Seoul National University, Seoul, South Korea, October 7, 2010.
  71. Research on Heat Transfer and Cooling of Gas Turbine Engine Components Including Measurement Techniques, Aero Propulsion Systems Department, Aeronautics Technology Division, KARI – Korea Aerospace Research Institute, Daejeon, South Korea, October 8, 2010.
  72. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Mechanical Engineering and Materials Science Department, School of Engineering and Applied Science, Washington University in St. Louis, St. Louis, Missouri, USA, December 2, 2010.
  73. Parks College of Engineering, Aviation, and Technology – Research Discussions at Scott Air Force Base, Air Mobility Command (AMC) – Scott Air Force Base, Scott Air Force Base, Illinois, USA, December 17, 2010.
  74. Parks College of Engineering, Aviation, and Technology – Research Activities, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, February 18, 2011.
  75. Parks College of Engineering, Aviation, and Technology – Graduate School Research Opportunities, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, February 23, 2011.
  76. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Distinguished Seminar Series, Department of Mechanical Engineering, Dwight Look College of Engineering, TAMU – Texas A&M University, College Station, Texas, USA, March 30, 2011.
  77. Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Including the Effects of Varying Tip Gap, CEAS Distinguished Lecture Series, Department of Mechanical Engineering, College of Engineering, University of Wisconsin-Milwaukee, Milwaukee, Wisconsin, USA, April 21, 2011.
  78. Science, Engineering, and Jet Engines, Physics Class, LaDue Horton Watkins High School, LaDue, Missouri, USA, May 11, 2011.
  79. Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Including the Effects of Varying Tip Gap, Turbomachinery and Heat Transfer Branch, NASA Glenn Research Center, Cleveland, Ohio, USA, June 28, 2011.
  80. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Department of Mechanical and Aerospace Engineering, U.S. Naval Postgraduate School, Monterey, California, USA, August 11, 2011.
  81. An Overview of Parks College of Engineering, Aviation, and Technology (with K. Ravindra), The Boeing Company, St. Louis, Missouri, USA, September 12, 2011.
  82. Saint Louis University – Parks College of Engineering, Aviation, and Technology – An Overview and Review of Research Opportunities, Department of Mechanical and Automotive Engineering, Inje University, Gimhae, Korea, October 31, 2011.
  83. Experimental Investigations of Jet Array Impingement Heat Transfer and Full-Coverage Film Cooling, Department of Mechanical and Automotive Engineering, Inje University, Gimhae, Korea, November 1, 2011.
  84. Experimental Investigations of Jet Array Impingement Heat Transfer and Full-Coverage Film Cooling, University of Science and Technology of China, Hefei, P. R. China, November 5, 2011.
  85. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, University of Michigan-Shanghai Jiao Tong University Joint Institute, Shanghai Jiao Tong University, Shanghai, P. R. China, November 7, 2011.
  86. Experimental Investigations of Jet Array Impingement Heat Transfer and Heat Transfer and Flow Structure On and Above Dimpled Surfaces, Mechanical Engineering Department, Tokyo University of Science, Tokyo, Japan, November 8, 2011.
  87. Experimental Investigations of Jet Array Impingement Heat Transfer and Heat Transfer and Flow Structure On and Above Dimpled Surfaces, DENSO Corporation, Nagoya, Japan. November 10, 2011.
  88. Experimental Investigations of Jet Array Impingement Heat Transfer, Full-Coverage Film Cooling, and Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Mitsubishi Heavy Industries, Takasago, Japan, November 15, 2011.
  89. Thermal-Fluid Sciences Research at Parks College of Engineering, Aviation, and Technology, The Boeing Company, St. Louis, Missouri, USA, October 21, 2011.
  90. Influence of Corners (With and Without Fillets) on Turbulent Boundary Layers with Transonic Shock Waves in Channels, The Boeing Company, St. Louis, Missouri, USA, December 19, 2011.
  91. Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Including the Effects of Varying Tip Gap, BEARS Seminar, Department of Mechanical Engineering, School of Engineering and Applied Science, Baylor University, Waco, Texas, USA, January 26, 2012.
  92. Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Including the Effects of Varying Tip Gap, Mechanical Engineering Department, Virginia Tech, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, USA, February 10, 2012.
  93. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – February 21, 2012, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, February 21, 2012.
  94. Parks College of Engineering, Aviation, and Technology – Graduate School Research Opportunities, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, March 28, 2012.
  95. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – May 8, 2012, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, May 8, 2012.
  96. Experimental Investigations of Full-Coverage Film Cooling and Over-Tip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer, Institute of Power Engineering, Department of Thermal Engineering, Tsinghua University, Beijing, P. R. China, May 24, 2012.
  97. Experimental Investigations of Jet Array Impingement Heat Transfer and Full-Coverage Film Cooling, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an, P. R. China, May 25, 2012.
  98. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Department of Mechanical Engineering, Graduate School of Engineering, Osaka University, Osaka, Japan, May 29, 2012.
  99. Investigations of Heat Transfer and Aerodynamic Phenomena as Applied to Turbine and Combustor Components of Gas Turbine Engines, IHI Corporation, Tokyo, Japan, May 30, 2012.
  100. Aerodynamic Losses in Turbines With and Without Film Cooling, as Influenced by Mainstream Turbulence, Surface Roughness, Airfoil Shape, and Mach Number, Department of Mechanical and Automotive Engineering, Advanced Vehicle Core Parts Research Group, Inje University, Republic of Korea, May 31, 2012.
  101. Slip Phenomena in Gases and a Newtonian Liquid as Investigated Within a Micro-Scale Viscous Disk Pump, Institute of Aerospace Thermodynamics (ITLR), Department of Aviation and Aerospace Engineering, University of Stuttgart, June 8, 2012.
  102. Investigations of Heat Transfer and Aerodynamic Phenomena as Applied to Turbine and Combustor Components of Gas Turbine Engines, Technology Department of Research and Development Center, AVIC Commercial Aircraft Engine Co., Ltd., Shanghai, P. R. China, September 13, 2012.
  103. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – August 23, 2012, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, August 23, 2012.
  104. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – September 25, 2012, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, September 25, 2012.
  105. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – October 15, 2012, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, October 15, 2012.
  106. International Grants and Interdisciplinary Grant Workshops (with D. Carlin, P. Turner), Frost Campus, Saint Louis University, St. Louis, Missouri, USA, November 30, 2012.
  107. International Grants and Interdisciplinary Grant Workshops (with D. Carlin, P. Turner), South Campus, Saint Louis University, St. Louis, Missouri, USA, November 30, 2012.
  108. International Grants and Interdisciplinary Grant Workshops (with D. Carlin, P. Turner), Frost Campus, Saint Louis University, St. Louis, Missouri, USA, December 3, 2012.
  109. International Grants and Interdisciplinary Grant Workshops (with D. Carlin, P. Turner), Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, January 30, 2013.
  110. Thermal-Fluid Sciences – Some Recent Research Activities (P. M. Ligrani), Aerospace Engineering and Mechanical Engineering Department, Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, February 28, 2013.
  111. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), School of Mechanical Engineering, Hanyang University, Seoul, Republic of Korea, March 27, 2013.
  112. Saint Louis University – Parks College of Engineering, Aviation, and Technology – An Overview and Review of Research Opportunities (P. M. Ligrani), School of Mechanical Engineering, Hanyang University, Seoul, Republic of Korea, March 27, 2013.
  113. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), Department of Mechanical and Automotive Engineering, Advanced Vehicle Core Parts Research Group, Inje University, Republic of Korea, March 29, 2013.
  114. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), Institute of Power Engineering, Department of Thermal Engineering, Tsinghua University, Beijing, P. R. China, April 1, 2013.
  115. Aerodynamic Losses in Turbines With and Without Film Cooling, as Influenced by Mainstream Turbulence, Surface Roughness, Airfoil Shape, and Mach Number (P. M. Ligrani), School of Mechanical Engineering, Northwestern Polytechnical University (NPU), Xi’an, P. R. China, April 3, 2013.
  116. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an, P. R. China, April 3, 2013.
  117. New Developments in Surface Heat Transfer Augmentation Technologies as Applied to Internal Flow Environments (P. M. Ligrani), The George W. Woodruff School of Mechanical Engineering, College of Engineering, Georgia Institute of Technology, Atlanta, Georgia, USA, April 24, 2013.
  118. Parks College of Engineering, Aviation, and Technology – Status of Graduate Programs – May 7, 2013 (P. M. Ligrani), Faculty Retreat – Parks College of Engineering, Aviation, and Technology, Saint Louis University, St. Louis, Missouri, USA, May 7, 2013.
  119. Jet Array Impingement Heat Transfer (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 14, 2013.
  120. Full Coverage Film Cooling for Combustor Liner Applications (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 14, 2013.
  121. Flow and Heat Transfer On and Near a Transonic Turbine Blade Tip (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 15, 2013.
  122. Micro-Fluidic Slip Phenomena in Gases and Liquids (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 15, 2013.
  123. Aerodynamic Losses In Turbines With and Without Film Cooling (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 16, 2013.
  124. Heat Transfer and Flow Structure On and Above Dimpled Surfaces in Macro- and Micro-Scale Channels (P. M. Ligrani), School of Energy and Power Engineering, Institute of Turbomachinery, Xi’an Jiaotong University, Xi’an, P. R. China, October 16, 2013.
  125. Heat Transfer and Flow Structure On and Above Dimpled Surfaces in Macro- and Micro-Scale Channels (P. M. Ligrani), School of Mechanical Engineering, Northwestern Polytechnical University (NPU), Xi’an, P. R. China, October 16, 2013.
  126. Recent Heat Transfer and Aerodynamics Research Developments For Application to Turbine Components of Gas Turbine Engines (P. M. Ligrani), Invited Lecture at the Opening Ceremony for the Institute of Gas Turbines of Beijing Tsinghua University, Beijing, P. R. China, February 27, 2014.
  127. Slip Phenomena in Gases and a Newtonian Liquid As Investigated Within a Micro-Scale Viscous Disk Pump (P. M. Ligrani), Department of Thermal Energy and Power Engineering, China University of Petroleum, Qingdao, P. R. China, March 3, 2014.
  128. Experimental Investigations of Jet Array Impingement Heat Transfer (P. M. Ligrani), Department of Thermal Energy and Power Engineering, China University of Petroleum, Qingdao, P. R. China, March 3, 2014.
  129. Slip Phenomena in Gases and a Newtonian Liquid As Investigated Within a Micro-Scale Viscous Disk Pump (P. M. Ligrani), Department of Mechanical Engineering, Yeungnam University, Republic of Korea, March 5, 2014.
  130. Experimental Investigations of Jet Array Impingement Heat Transfer (P. M. Ligrani), Department of Mechanical and Automotive Engineering, Advanced Vehicle Core Parts Research Group, Inje University, Republic of Korea, March 6, 2014.
  131. Investigation of Shock Wave Boundary Layer Interactions in a Newly Developed 3.57 Aspect Ratio Wind Tunnel (P. M. Ligrani), Department of Aeronautics, Imperial College London, South Kensington, London, United Kingdom, June 13, 2014.
  132. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), Institute of Particle Science and Engineering, School of Chemical and Process Engineering, University of Leeds, Leeds, England, United Kingdom, June 16, 2014.
  133. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), B&B-AGEMA GmbH, Aachen, Germany, June 20, 2014.
  134. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), Institut für Thermische Stroemungsmaschinen, Karlsruher Institut für Technologie (KIT), Karlsruhe, Germany, June 23, 2014.
  135. Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), ITLR-Institute of Aerospace Thermodynamics, University of Stuttgart, Stuttgart, Germany, June 25, 2014.
  136. Aerodynamics Loss Investigations of Turbine Components, Including Aero-Thermodynamic and Film Cooling Influences (P. M. Ligrani), Institute of Power Engineering, Department of Thermal Engineering, Tsinghua University, Beijing, P. R. China, September 19, 2014.
  137. Heat Transfer Augmentation Technologies For Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 20, 2014.
  138. Heat Transfer and Flow Structure On and Above Dimpled Surfaces in Macro- and Micro-Scale Channels (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 20, 2014.
  139. Aerodynamics Losses in Turbines With and Without Film Cooling, as Influenced by Mainstream Turbulence, Surface Roughness, Airfoil Shape, and Mach Number (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 21, 2014.
  140. Jet Array Impingement Heat Transfer – Part 1: 1. Effects of Jet-to-Target Plate Distance and Reynolds Number, 2. Effects of Hole Spacing and Reynolds Number (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 21, 2014.
  141. Jet Array Impingement Heat Transfer – Part 2: 3. Separate Effects of Mach Number and Reynolds Number (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 22, 2014.
  142. Flow and Heat Transfer On and Near a Transonic Turbine Blade Tip – Including Effects of a Varying Tip Gap (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 22, 2014.
  143. Full Coverage Film Cooling for Combustor Liner Applications, Part 1 – Heat Transfer Coefficients and Film Effectiveness for a Sparse Hole Array at Different Blowing Ratios and Contraction Ratios (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 23, 2014.
  144. Full Coverage Film Cooling for Combustor Liner Applications, Part 2 – Comparisons Between Sparse and Dense Hole Arrays at Different Blowing Ratios and Contraction Ratios (P. M. Ligrani), School of Energy and Power Engineering, Beihang University, BUAA – Beijing University of Aeronautics and Astronautics, Beijing, P. R. China, September 23, 2014.
  145. Heat Transfer and Aerodynamics Research For Gas Turbines and Other Propulsion Systems (P. M. Ligrani), Eminent Scholar Inaugural Seminar, Eminent Scholar in Propulsion, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, January 23, 2015.
  146. Heat Transfer and Aerodynamics Research For Gas Turbines and Other Propulsion Systems (P. M. Ligrani), Propulsion Systems Department, NASA – MSFC, NASA – Marshall Space Flight Center, Huntsville, Alabama, USA, April 9, 2015.
  147. Supersonic Flow Research at the Propulsion Research Center (P. M. Ligrani), The Boeing Company Visit, Propulsion Research Center, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, April 21, 2015.
  148. Supersonic Flow Research at the Propulsion Research Center (P. M. Ligrani), Northrop Grumman Corp. Visit, Propulsion Research Center, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, April 29, 2015.
  149. Heat Transfer and Aerodynamics Research For Gas Turbines and Other Propulsion Systems (P. M. Ligrani), Propulsion and Structures Division, AMRDEC – Aviation and Missile Research, Development and Engineering Center, RDECOM – U. S. Army Research, Development, and Engineering Command, Redstone Arsenal, U. S. Army, Huntsville, Alabama, USA, May 7, 2015.
  150. Welcome to the University of Alabama in Huntsville (P. M. Ligrani), Symposium on Gas Turbine Technology and Research, Beijing Tsinghua University Visit, Mechanical and Aerospace Engineering Department, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, May 11, 2015.
  151. Recent Progress and Future Directions of Gas Turbine Research (P. M. Ligrani), Symposium on Gas Turbine Technology and Research, Beijing Tsinghua University Visit, Mechanical and Aerospace Engineering Department, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, May 11, 2015.
  152. Heat Transfer Augmentation Technologies For Internal Cooling of Turbine Components of Gas Turbine Engines (P. M. Ligrani), School of Energy and Power, DLUT – Dalian University of Technology, Dalian, P. R. China, July 7, 2015.
  153. Heat Transfer and Flow Structure On and Above Dimpled Surfaces in Macro- and Micro-Scale Channels (P. M. Ligrani), School of Energy and Power, DLUT – Dalian University of Technology, Dalian, P. R. China, July 7, 2015.
  154. Aerodynamics Losses in Turbines With and Without Film Cooling, as Influenced by Mainstream Turbulence, Surface Roughness, Airfoil Shape, and Mach Number (P. M. Ligrani), School of Energy and Power, DLUT – Dalian University of Technology, Dalian, P. R. China, July 8, 2015.
  155. Flow and Heat Transfer On and Near a Transonic Turbine Blade Tip – Including Effects of a Varying Tip Gap (P. M. Ligrani), School of Energy and Power, DLUT – Dalian University of Technology, Dalian, P. R. China, July 8, 2015.
  156. Over-Tip Shock Wave Structure and Its Impact On Turbine Blade Tip Heat Transfer, Including the Effects of a Varying Tip Gap (P. M. Ligrani), Institute of Power Engineering, Department of Thermal Engineering, Beijing Tsinghua University, Beijing, P. R. China, July 9, 2015.
  157. Heat Transfer and Aerodynamics Research for Gas Turbines and Other Propulsion Systems (P. M. Ligrani), National Gas Turbine Research Center, Beijing Tsinghua University, Beijing, P. R. China, July 10, 2015.
  158. Effects of Target Surface Roughness on Jet Array Impingement Heat Transfer (P. M. Ligrani, Zhong Ren, and Warren Buzzard), IHI Corporation, Yokohama, Japan, July 15, 2015.
  159. Thermal-Fluid Sciences Research Capabilities at the University of Alabama in Huntsville (P. M. Ligrani), IHI Corporation, Yokohama, Japan, July 15, 2015.
  160. Microfluidics and Microplasmas for Space Micro-Propulsion (G. Xu, and P. M. Ligrani), NASA – Marshall Space Flight Center, Huntsville, Alabama, USA, May 29, 2015.
  161. Microfluidics and Microplasmas for Space Micro-Propulsion (G. Xu, and P. M. Ligrani), The Boeing Company, Huntsville, Alabama, USA, June 12, 2015.
  162. SS/TS/WT SuperSonic/TransSonic/WindTunnel for Advanced Aerospace and Aeropropulsion Research (P. M. Ligrani), Propulsion Research Center, University of Alabama in Huntsville, Huntsville, Alabama, USA, September 18, 2015.
  163. Over-Tip Shock Wave Structure and Its Impact On Turbine Blade Tip Heat Transfer, Including the Effects of a Varying Tip Gap (P. M. Ligrani), Department of Mathematics, University of Texas at Arlington, Arlington, Texas, USA, November 6, 2015.
  164. UAH PRC MAE SS/TS/WT Facility – SuperSonic/TransSonic/ WindTunnel Laboratory Capabilities (P. M. Ligrani), Propulsion Research Center, University of Alabama in Huntsville, Huntsville, Alabama, USA, January 29, 2016.
  165. Research Highlights and New Developments at the Propulsion Research Center (P. M. Ligrani), Engineering Advisory Board Meeting, College of Engineering, University of Alabama in Huntsville, Huntsville, Alabama, USA, February 19, 2016.
  166. Recent Research Developments in Gas Turbine Cooling: (1) Double Wall Cooling With Impingement Cooling and Full Coverage Effusion Cooling, and (2) Influences of Target Surface Roughness on Impingement Jet Array Heat Transfer (P. M. Ligrani), KIMM – Korea Institute of Machinery and Materials, 156, Gajeongbuk-Ro, Yuseong-Gu, Daejeon, South Korea, June 17, 2016.
  167. Recent Research Developments in Gas Turbine Cooling: (1) Double Wall Cooling With Impingement Cooling and Full Coverage Effusion Cooling, and (2) Influences of Target Surface Roughness on Impingement Jet Array Heat Transfer (P. M. Ligrani), Institute of Thermal Turbomachinery, KIT – Karlsruhe Institute of Technology, Karlsruhe, Germany, July 22, 2016.
  168. Effects of Double Wall Cooling Configuration and Conditions on Internal and External Cooling of a Full Coverage Effusion Plate (P. M. Ligrani), Solar Turbines, Inc., San Diego, California, USA, September 9, 2016.
Copyright Trademarks Ligrani Research Group 2009