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验证码:

Dr. John Schmisseur

职称:Professor

所属学校:The University of Tennessee-Knoxville

所属院系:Industrial Engineering

所属专业:Industrial Engineering

联系方式:(931) 393-7274

简介

B.S. Aerospace Engineering, The University of Texas at Austin, 1990 M.S. Aerospace Engineering, The University of Texas at Austin, 1992 Thesis: “An Experimental Study of Fluctuating Wall Pressures in a Highly Swept, Sharp Fin-Induced, Mach 5 Shock Wave/Turbulent Boundary Layer Interaction”; advisor: D.S. Dolling Ph.D., Dept. of Aeronautics and Astronautics, Purdue University, 1997 Dissertation: “Receptivity of the Boundary Layer on a Mach-4 Elliptic Cone to Laser-Generated Localized Freestream Perturbations”; advisor: S.P. Schneider Department of Defense Acquisition Professional Development Program º Level III Certified in Science and Technology Management, 2012

职业经历

2013-2014: Chief of the Energy, Power & Propulsion Sciences Division - Responsible for division strategic direction, fiscal performance, personnel development and management, and coordination with other agencies. 2001-2014: Program Manager, Air Force Office of Scientific Research - Responsible for the strategic direction, development, execution and communication of Air Force basic research in high-speed aerodynamics and the related scientific disciplines º Program Manager for Aerothermodynamics and Turbulence: 2001-2014 º Program Manager for Flow Control and Aeroelasticity: 2005, 2007-2009 º Program Manager for Test and Evaluation: 2006-2007, 2008 1998-2001: Research Aerospace Engineer, Computational Sciences Branch, Air Vehicles Directorate. Numerical simulation of viscous hypersonic flows. 1997-1998: Research Aerospace Engineer, Experimental Operations and Diagnostics Branch, Air Vehicles Directorate. Experimental investigation of supersonic viscous flows. 1993-1997: Doctoral Student at Purdue University, supported by USAF Palace Knight Program. Conducted experimental investigation of supersonic boundary-layer transition and developed optical perturbation technique for high-speed wind tunnels. 1992-1993: Aerospace Engineer, Optical Diagnostics Group, Air Vehicles Directorate. Developed and applied optical diagnostic methods for hypersonic flows. 1991-1992; Masters degree candidate at The University of Texas at Austin, supported by USAF Palace Knight Program. Conducted experimental investigation of shock wave/turbulent boundary layer interactions.

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