Publications list David Munday

Transcription

1 Publications Peer-reviewed Archival Journals 1. Experimental Study of a Multi-nozzle Combustor at Elevated Pressures, Villalva, R., Dolan, B., Munday, D., Zink, G., Pack, S., Goeke, J., Gutmark, E., Submitted to AIAA Journal. 2. Experimental Comparison of Axial Turbine Performance Under Steady and Pulsating Flows, St. George, A., Driscoll, R., Gutmark, E., Munday, D., Submitted to Journal of Turbomachinery. 3. Supersonic Turbojet Noise Reduction, Munday, D., Cuppoletti, D., Perrino, M., Gutmark, E., Burak, M. and Eriksson, L-E., International Journal of Aeroacoustics Vol. 12, No. 3, June 2013, pp Effect of the Initial Turbulence Level on An Underexpanded Supersonic Jet, Liu, J., Kailasanath, L., Boris, J., Heeb, N., Munday, D., Gutmark, E., AIAA Journal, Vol. 51, No. 3, March 2013, pp Acoustic Effect of Chevrons on Supersonic Jets Exiting Conical C-D Nozzles, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., AIAA Journal, Vol. 50, No. 11, Nov 2012, pp Experimental and Numerical Investigation of a Supersonic C-D Nozzle, Burak, M., Eriksson, L-E., Munday, D., Gutmark, E. and Prisell, E., AIAA Journal, Vol. 50, No. 7, July 2012, pp Flow structure and acoustics of supersonic jets from conic convergent-divergent nozzles, Munday, D., Gutmark, E., Liu, J., Kailasanath, K., Physics of Fluids, Vol. 23, No. 11, Nov 2011, pp Supersonic Jet Noise Reduction Technologies for Gas Turbine Engines, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., Journal of Engineering for Gas Turbines and Power, Vol. 133, No. 10, Oct 2011, pp Experimental and Numerical Study of Jets from Elliptic Nozzles with Conic Plug, Munday, D., Mihaescu, M., Gutmark, E., AIAA Journal, Vol. 49, No. 3, March 2011, pp Large-Eddy Simulations of a Supersonic Jet and Its Near-Field Acoustic Properties, Liu, J., Kailasanath, K., Ramamurti, R., Munday, D., Gutmark, E., Lohner, R., AIAA Journal, Vol. 47, 2009, pp (Received Alan Berman Research Publication Award from Naval Research Laboratory) 11. Active Control of Separation on a Wing with Oscillating Camber, Munday, D., Jacob, J., Huang, G., Journal of Aircraft, Vol. 39, No. 1, No. 8, 2002, pp Conference Papers 1. Experimental Comparison of Axial Turbine Performance Under Pulsed-Air and Pulsed-Detonation Flows, St. George, A., Driscoll, R., Munday, D., Gutmark, E., 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, July. 2. Thermodynamic and Visualization Study of Shock Transfer in a Dual Pulse Detonation-Crossover System, Driscoll, R., St. George, A., Stoddard, W., Munday, D., Gutmark, E., 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, July. 3. Biofuel Emissions of a Multipoint Staged Low NOX Combustion System at Intermediate Pressures, Dolan, B., Villalva, R., Munday, D., Gutmark, E., Zink, G., Ryon, J., Pack, S., Goeke, J., 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, July. Page 1 of 8

2 4. Medium Pressure Emissions of a Multi-point Low NOx Combustion System, Villalva, R., Dolan, B., Munday, D., Gutmark, E., Zink, G., Ryon, J., Pack, S., Goeke, J., ASME Turbo Expo 2013, San Antonio, Texas, 3-7 June 2013, GT Computational Study of Shock-Associated Noise Characteristics Using LES, Liu, J, Corrigan, A., Kailasanath, K., Heeb, N., Munday, D., Gutmark, E., 19th AIAA/CEAS Aeroacoustics Conference, Berlin, Germany, May 2013, AIAA DOI: / The Design and Validation of a Pulse Detonation Engine Facility with and without Axial Turbine Integration, Munday, D., St. George, A., Driscoll, R., Stoddard, W., Romanchuk, B., Gutmark, E., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA Experimental Investigation of Axial Turbine Performance Driven by Steady and Pulsating Flows, St. George, A., Driscoll, R., Stoddard, W., Munday, D., Gutmark, E., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA Impact of Deck and Jet Blast Deflector on the Flow and Acoustic Properties of Imperfectly Expanded Supersonic Jets, Liu, J., Kailasanath, K., Heeb, N., Munday, D., Gutmark, E., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA OH* Chemiluminescence in a Multipoint Combustion System: Steady State and Limit Cycle Behavior, Dolan, B, Villalva Gomez, R., Munday, D., Gutmark, E., Zink, G., Pack, S., Goeke, J., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA Medium Pressure Emissions of a Multipoint Low NOx Combustion System, Villalva Gomez, R., Dolan, B., Munday, D., Gutmark, E., Zink, G., Pack, S., Goeke, J., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA Experimental Study of Sustained Shock Initiated Detonation in a Multiple Pulse Detonation-Crossover System, Driscoll, R., Stoddard, W., St. George. A., Munday, D., Gutmark, E., 51st AIAA Aerospace Sciences Meeting, Grapevine, TX 7-10 Jan 2013, AIAA Techniques for Turbojet Noise Reduction, Munday, D., Cuppoletti, D., Perrino, M., Gutmark, E., Burak, M, Eriksson, L., ASME Turbo Expo 2012, Copenhagen, Denmark, June 2012, GT Effect of Nozzle-exit Flow Conditions on the Flow and Acoustic Properties of Imperfectly Expanded Supersonic Jets, Liu, J., Kailasanath, K., Boris, J., Heeb, N., Munday, D., Gutmark, E., 18 th AIAA/CEAS Aeroacoustics Conference (33 rd AIAA Aeroacoustics Conference), Colorado Springs, Colorado, 4-6 June 2012, AIAA The Impact of Heat on the Near and Far-Field Pressure Skewness in Supersonic Jets, Mora, P., Kastner, J., Heeb, N., Munday, D., Gutmark, E., Liu, J., Kailasanath, K., 50 th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, 9-12 January 2012, AIAA Parametric Study of Direct Detonation Initiation from Shock Transfer through a Crossover Tube, Driscoll, R., Stoddard, W., St. George, A., Romanchuk, B., Munday, D., Gutmark, E., 50 th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, 9-12 January 2012, AIAA Dual Crossover Dual Shock Ignition of a Pulse Detonation Engine, Stoddard, W., Driscoll, R., St. George, A., Romanchuk, B., Munday, D., Gutmark, E., 50 th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, 9-12 January 2012, AIAA Supersonic Jet Noise Reduction using Fluidics, Mechanical Chevrons and Fluidically Enhanced Chevrons, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., ASME Turbo Expo 2010, Glasgow, Scotland, June 2010, GT (Selected for Aircraft Engine Best Paper Award) Page 2 of 8

3 18. Large-Eddy Simulations of a Supersonic Heated Jet, Liu, J., Kailasanath, K., Heeb, N., Munday, D., Gutmark, E., 17 th AIAA/CEAS Aeroacoustics Conference (32 rd AIAA Aeroacoustics Conference), Portland, Oregon, 5-8 June 2011, AIAA Proper Orthogonal Decomposition Analysis of Numerically Simulated Supersonic Jet Flow, Mignee, J., Kastner, J., Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., 40th Fluid Dynamics Conference and Exhibit, Chicago, Illinois, 28-1 June, 2010, AIAA Supersonic Jet Noise Reduction by Chevrons Enhanced with Fluidic Injection, Heeb, N., Munday, D., Gutmark, E., Liu, J., Kailasanath, K., 40th Fluid Dynamics Conference and Exhibit, Chicago, Illinois, 28-1 June, 2010, AIAA Fluidic Injection for Noise Reduction of a Supersonic Jet from a practical C-D nozzle, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., 16 th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 7-9 June 2010, AIAA Large-Eddy Simulations of a Supersonic Jet with Fluidic Injection for Noise Reduction, Liu, J., Kailasanath, K., Ramamurti, R., Munday, D., Gutmark, E., 16 th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 7-9 June 2010, AIAA Comparison of Flow Control Methods Applied to Conical C-D Nozzles, Munday, D., Heeb, N., Perrino, M., Gutmark, E., Heeb, N., Burak, M, Eriksson, L., Prisell, E., 16 th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 7-9 June 2010, AIAA Micro-jet flow control for noise reduction of a supersonic jet from a practical C-D nozzle, Perrino, M., Munday, D., Gutmark, E., Heeb, N., Burak, M, Eriksson, L., Prisell, E., 16 th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 7-9 June 2010, AIAA Near-Field Jet Noise from a Supersonic C-D Chevron Nozzle, Burak, M, Eriksson, L., Munday, D., Gutmark, E., Prisell, E., 16 th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 7-9 June 2010, AIAA Forward flight effects on the shock structure from a chevron C-D nozzle, Munday, D., Gutmark, E., Heeb, N., Burak, M, Eriksson, L., Prisell, E., 48 th AIAA Aerospace Sciences Meeting, 5 Jan 2010, Orlando FL, AIAA An Application of Commercial Noise Reduction Techniques to Military Aircraft Nozzles, Heeb, N., Munday, D., Gutmark, E., Liu, J., Kailasanath, K., 48 th AIAA Aerospace Sciences Meeting, 5 Jan 2010, Orlando FL, AIAA Flow Structure of Supersonic Jets from Conical C-D Nozzles, Munday, D., Gutmark, E., Liu, J., Kailasanath, K., 39 th AIAA Fluid Dynamics Conference, 24 June 2009, San Antonio, Texas, AIAA Experimental and Numerical Investigation of a Supersonic C-D Chevron Nozzle, Burak, M, Eriksson, L., Munday, D., Gutmark, E., Prisell, E., 39th AIAA Fluid Dynamics Conference, San Antonio, Texas, June 22-25, 2009, AIAA Impact of Mechanical Chevrons on Supersonic Jet Flow and Noise, Kailasanath, K., Liu, J., Gutmark, E., Munday, D., Martens, S., ASME Turbo Expo 2009, 8-12 June 2009, Orlando, FL, ASME-GT Acoustic Effect of Chevrons on Jets Exiting Conical C-D Nozzles, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., 15 th AIAA/CEAS Aeroacoustics Conference, 11 May 2009, Miami, FL, AIAA Page 3 of 8

4 32. Large-Eddy Simulations of Imperfectly Expanded Jets from a Chevron Nozzle, Liu, J., Kailasanath, K., Ramamurti, R., Munday, D., Gutmark, E., 15 th AIAA/CEAS Aeroacoustics Conference, 11 May 2009, Miami, FL, AIAA Experimental and Numerical Investigation of a Supersonic C-D Nozzle, Burak, M, Eriksson, L., Munday, D., Gutmark, E., Prisell, E., 15 th AIAA/CEAS Aeroacoustics Conference, 12 May 2009, Miami, FL, AIAA Supersonic Jet Noise from a Conical C-D nozzle with Forward Flight Effects, Munday, D., Heeb, N., Gutmark, E., Burak, M., Eriksson, L., Prisell, E., 47 th AIAA Aerospace Sciences Meeting, 5 Jan 2009, Orlando FL, AIAA Large-Eddy Simulation of a Supersonic Jet and Its Near-Field Acoustic Properties :Methodology and Validation, Liu, J., Kailasanath, K., Ramamurti, R., Munday, D., Gutmark, E., Lohner, R., 47 th AIAA Aerospace Sciences Meeting, 5 Jan 2009, Orlando FL, AIAA Investigation of Near-Field Acoustic Properties of Imperfectly Expanded Jet Flows Using LES, Liu, J., Kailasanath, K., Munday, D., Gutmark, E., 47 th AIAA Aerospace Sciences Meeting, 5 Jan 2009, Orlando FL, AIAA Large Eddy Simulation for Turbulent Mixing in Elliptic Jets with Round Center-Body, Mihaescu, M., Munday, D., Gutmark, E., 47 th AIAA Aerospace Sciences Meeting, 5 Jan 2009, Orlando FL, AIAA Flow and Acoustic Radiation from Realistic Tactical Jet C-D Nozzles, Munday, D., Gutmark, E., Liu, J., Kailasanath, K., 14 th AIAA/CEAS Aeroacoustics Conference, 5 May 2008, Vancouver, British Columbia, Canada, AIAA Development of a Jet from an Elliptic Nozzle with Round Centerbody, Munday, D., Gutmark, E., 46 th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada, AIAA Jet Aircraft Propulsion Noise Reduction Research at University of Cincinnati, Rask, O., Harrison, S., Munday, D., Harris, C., Mihaescu, M., Gutmark, E., 43 rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 8-11, 2007, Cincinnati, OH, AIAA Experimental and Numerical Investigation of Aerodynamic Flow Control Using Oscillating Adaptive Surfaces, Munday, D., Jacob, J., Hauser, T., Huang, G., AIAA First Flow Control Conference, June 2002, St. Louis, Missouri. 42. Active Flow Control of Separation on a Wing with Oscillatory Camber, Munday, D., Jacob, J., Huang, G., Fortieth AIAA Aerospace Sciences Meeting and Exhibit, January 2002, Reno, Nevada, AIAA "Active Control of Separation on a Wing with Conformal Camber," Munday, D., Jacob, J., AIAA Thirty- Ninth Annual Aerospace Sciences Meeting, 8-11 January 2001, Reno, Nevada, AIAA "Flow Control Experiments for low Re Adaptive Airfoils," Munday, D., Jacob, J. D., AIAA, Thirty-Eighth Annual Aerospace Sciences Meeting, 12 January 2000, Reno, Nevada, AIAA Conference Talks 1. Design of a pulse detonation engine facility with and without axial turbine integration, Munday, D., Driscoll, R., St. George, A., Romanchuk, B, Stoddard, W., Gutmark, E., 37 th Annual Dayton-Cincinnati Aerospace Sciences Symposium, 5 March 2012, Dayton, Ohio. Page 4 of 8

5 2. Investigation of the Near-Field Acoustic Properties of Supersonic Jets with Fluidic Enhanced Chevrons using Large-Eddy Simulations, Liu, J., Kailasanath, K., Ramamurti, R. Heeb, N., Munday, D., Gutmark, Sixty-Third Annual Meeting of the American Physical Society, Division of Fluid Mechanics, November 2010, Long Beach, CA. 3. Mechanical Chevrons and Fluidics for Military Jet Aircraft Noise Reduction, Kastner, J., Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K. and Ramamurti, R. Turbine Engine Technology Symposium (TETS 2010) Sept 2010, Dayton, Ohio. 4. Investigation of the Acoustic Properties of Supersonic Jets with Fluidic Injection on Chevrons: Experimental Results, Munday, D., Heeb, N., Gutmark, E., Liu, J., Kailasanath, K., Sixty- Second Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 24 November 2009, Minneapolis, Minnesota. 5. Elliptic jets: Laboratory and practical configurations, Gutmark, E., Munday, D., Mihaescu, M., The 2nd International Conference on Jets, Wakes and Separated Flows, 16 September 16, 2008, Berlin, Germany. 6. Acoustic Radiation from Imperfectly Expanded Supersonic Jets; Experimental Investigation, Munday, D., Gutmark., Liu, J., Kailasanath, K., Sixtieth Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 19 November 2007, Salt Lake City, Utah. 7. The Hypersonic Lego: Getting Started with Pressure Sensitive Paint, Munday. D., Fletcher, D., Fifty- Sixth Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 25 November 2003, East Rutherford, New Jersey. 8. "Low-Re Separation Control by Periodic Suction Surface Motion," Munday, D., Jacob, J. D., Fifty-Fifth Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 24 November 2002, Dallas, Texas. 9. "Low-Re Separation Control by Periodic Suction Surface Motion, Munday, D., Jacob, J. D., "Fifty-Fourth Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 19 November 2001, San Diego, California. 10. "Development of High-Lift Adaptive Airfoils for Low-Density Environments," Munday, D., Jacob, J. D., Seventh Annual Kentucky EPSCoR Conference, 8 May 2001, Bowling Green, Kentucky. 11. "Low-Reynolds-Number Separation Control using Adaptive Airfoils," Munday, D., Jacob, J. D., The AIAA 26th Annual Dayton-Cincinnati Aerospace Science Symposium, 30 March 2001, Dayton, Ohio. 12. "Active Separation Control at Low Re on a Wing with Conformal Camber," Munday, D., Jacob, J. D., Fifty-Third Annual Meeting of the American Physical Society, Division of Fluid Mechanics, 19 November 2000, Washington, DC. 13. "Adaptive Airfoil Research at University of Kentucky," Munday, D., Jacob, J. D., Sixth Annual EPSCoR Conference, 15 May 2000, Frankfort, Kentucky. 14. "Aerodynamic Flow Control using Adaptive Airfoils," Munday, D., Jacob, J. D., AIAA, Twenty-Fifth Annual Dayton-Cincinnati Aerospace Science Symposium, 30 March 2000, Dayton, Ohio. Conference Posters 1. Double Diamonds and the Sound of Freedom: Jet Flows and Acoustic Emissions from Practical Military Engine Nozzles, Munday, D., Heeb, N., Gutmark, E., Kailasanath, K., Liu, J., University of Cincinnati Graduate School, 2010 Poster Forum, Cincinnati, Ohio, 5 March (Selected as Best Poster in Physical Science and Engineering) Page 5 of 8

6 2. Mechanical Chevrons and Fluidics for Military Aircraft Noise Reduction, Kailasanath, K., Liu, J. Ramamurti, R., Gutmark, Ephraim, Munday, David and Martens, Steven, SERDP/ESTCP Partners in Environmental Technology Symposium, Washington, DC, Dec 1-3, Aerodynamic Flow Control Using Shape Adaptive Surfaces, Munday, D., Jacob, J. D., AIAA First Flow Control Conference, June 2002, St. Louis, Missouri. 4. Low-Speed Morphing Wing Flow Control,, Munday, D., Jacob, J. D., Seventh Annual Kentucky EPSCoR Conference, 7-8 May 2001, Bowling Green, Kentucky. 5. "Separation Control and L/D Improvement with a Conformally Cambered Wing," Munday, D., Jacob, J. D., AIAA, Fluids 2000 Conference and Exhibit, June 2000, Denver, Colorado. Technical Reports 1. Active Suppression of Jet Engine Noise, UC-CTH-FMV Joint Project ( A ) to Försvarets materielverk (FMV), (Principal author). 2. Mechanical Chevrons and Fluidics for Advanced Military Aircraft Noise Reduction, SERDP Project Number: WP-1584 (Second author). 3. Propulsion 21 Final Technical Report, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, Ohio, (Editor: Section 2.2, Author: Section 2.2.2). 4. Investigation of Pressure Sensitive Paints for High Speed Applications, Munday, D., von Karman Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium, June 2003 VKI-PR Service Journal Reviewer for AIAA Journal; Royal Aeronautical Society s Aeronautical Journal Conference Reviewer for ASME Turbo Expo Proposal Reviewer for: NASA EPSCoR 2012 University of Cincinnati Cincinnati Ohio, Jan 2011 present Parent Tour Committee Fire Science Curriculum Committee University of Kentucky Lexington, Kentucky, June August 1999 College of Engineering Curriculum Committee Aided in the development of a new Freshman Engineering course (EGR199). Wrote lessons for the associated computer lab. Proposals $90,000, General Electric Transportation (Aug 2013 Dec 2013) GE Rotating Detonation System Development Submitted: 26 Aug 2013, PI: Gutmark, E. (50%), Munday, D. (50%), Funded $258,746, General Electric Aviation (Aug 2013 July 2014) Page 6 of 8

7 Film Cooling Test Program Submitted: 19 July 2013, PI: Munday, D. (50%), CI: Gutmark, E. (50%) Pending $100,001, Innovative Scientific Solutions, Inc. (AFOSR) (Aug 2013 Jan 2014) Pulse Detonation Engine (PDE) Driven Turbine, Phase III Submitted: 15 July 2013, PI: Munday, D. (50%), CI: Gutmark, E. (50%), Pending $75,000, Combustion Research & Flow Technology Inc (DARPA) (1 Sept June 2014) Modeling and Optimizing Turbines for Unsteady Flow Submitted 21 March 2013, PI Gutmark (50%), CI: Munday, D. (50%) Pending $277,637, National Science Foundation (Sept 2013 August 2016) Low Emissions High Oxidation Temperature Distributed (Flameless) Combustion for Gas Turbines Submitted: 19 February 2013, PI: Munday, D. (50%), CI: Gutmark, E (50%),, Declined $45,000, Spectral Energies (ONR) (Jun 2013 May 2013) Screech Reduction by Open Loop Fuel Modulation and Symmetry Breaking Submitted: 15 Jan 2013, PI: Munday, D. (50%), CI: Gutmark, E. (50%), Pending $176,329, Halliburton Energy Services (Apr 2013 Nov 2013) MCS Port Geometry Concept Development Submitted: 11 Jan 2013, PI: Gutmark, E (50%), CI: Munday, D. (50%), Funded $37,950, Spectral Energies(ONR) (April 2013 Sept 2013) Distributed control of Multi-point Lean Direct Ignition System Submitted 28 November 2012, PI: Munday, D. (50%), CI: Gutmark, E (50%), Declined $50,000, Innovative Scientific Solutions, Inc. (AFOSR) (Nov 2012 Feb 2013) Pulse Detonation Engine (PDE) Driven Turbine, Phase IIb Submitted: 24 Oct 2012, PI: Munday, D. (50%), CI: Gutmark, E. (50%), Funded $58,467, Halliburton Energy Services (August 2012 Dec 2012) Autonomous Inflow Control Devices, Phase 1-2 Submitted: 1 August 2012, PI: Gutmark, E. (50%), CI: Munday, D. (50%), Funded $176,329, Halliburton Energy Services (July 2012 Nov 2012) Phase 2 Product Development Submitted 23 July 2012, PI: Gutmark, E. (50%), CI: Munday, D. (50%), Funded $49,999, Innovative Scientific Solutions, Inc. (AFOSR) (June 2012 Sept 2012) Pulse Detonation Engine (PDE) Driven Turbine Submitted: 13 June 2012, PI: Munday, D. (50%), CI: Gutmark, E. (50%), Funded $383,647, General Electric Aviation (June 2012 May 2013) Turbine Airfoil Cascade Test Submitted: 4 May 2012, PI: Gutmark, E. (33.4%), CI: Munday, D. (33.3%), Kastner, J. (33.3%), Funded $278,076, Ohio Department of Transportation (July 2012 June 2013) Comparison and Testing of Various Noise Wall Materials Submitted: 21 March 2012, PI: Swanson, J. (34%), CI: Rassati, G.A. (33%), CI: Munday, D (33%), Declined $150,000, Technical University Berlin (March 2012 Aug 2013) Wet Combustion at Elevated Pressure Submitted: 30 June 2011, PI: Munday, D. (50%), CI: Gutmark, E. (50%), Declined $50,000, Aero Systems Engineering (AFOSR) (Dec 2011, July 2012) Revolutionary Technologies for the Reduction of Aircraft Jet Noise Submitted 15 June 2011, PI: Gutmark, E. (50%), CI: Munday, D. (25%), CI: Kastner, J. (25%), Declined Page 7 of 8

8 $463,957, Department of the Navy (Aug 2011 Jul 2014) Active Air Powered Noise Control in Hot Supersonic Jets Submitted: 25 Feb 2011, PI: Gutmark, E. (25%), CI: Munday, D. (50%), CI: Kastner, J. (25%), Declined Other Professional Experience Munday Computing, Inc Florence, Kentucky, September July 1997 President/Chief Consultant Spurgeon Computing Cincinnati, Ohio, May August 1986 Programmer/Analyst Image One Systems Cincinnati, Ohio, June April 1985 Programmer/Analyst Leadership/Community Service Fairview-Clifton German Language School (Public Elementary School) Instructional Leadership Team (ILT), Sept 2012 present Fasching Festival Volunteer, Annually from 2008 Classroom parent help, Sept 2007 May 2008 Civil Air Patrol, Kentucky Wing Incident Commander, Qualified: March 04 Check Pilot (SAR/DR), Qualified: April 04 Director of Emergency Services, March 02 Sept 02 Flight Release Officer, May 00 Sept 02 Counter-Narcotics Pilot, Qualified: June 01 Air Operations Director, Qualified: March 01 Search and Rescue/Disaster Relief Pilot, Qualified: Feb 01 Cadet Orientation Pilot, Qualified: March 00 Civil Air Patrol, Campbell County Composite Squadron (Sq. KY-073) Deputy Commander, March 01 March 02 Flight Operations Officer, July 00 March 01 Experimental Aircraft Association, Waynesville Chapter (Chapter 284) President, Jan 94 Dec 95 Vice President, Jan 93 Dec 93 Tau Kappa Epsilon Fraternity, Pi-Omicron Chapter President, Apr 84 Apr 85 Vice President, May 83 Apr 84 Pledge Trainer, Apr 85 Apr 86 Treasurer Student Government, Northern Kentucky University Chief Justice, Judicial Council, Apr 84 Jan 85 Student Representative, Apr 83 Apr 84 Page 8 of 8