Ph.D. Mechanical Engineering, The Ohio State University, 1994 M.S. Mechanical Engineering, The Ohio State University, 1991 B.S. Mechanical Engineering, West Virginia University, 1989, Summa Cum Laude
Fluid Dynamics, Experimental Measurement Techniques, Mixing Technology
Reynolds, T. and Reeder, M., “Effect of Aspect Ratio on Flow through Serpentine Nozzles,” AIAAJournal of Aircraft, Vol. 49, No. 3, pp. 836-851, May 2012.
Thomas, L., Branam, R., and Reeder, M., “Flow Measurements Using Particle Image Velocimetry in theUltra Compact Combustor,” International Journal of Aerospace Engineering,” Vol. 2012, ArticleID 756463, 13 pages, 2012. doi:10.1155/2012/756463.
Curtis, D., Reeder, M., Svanberg, C., Cobb, R & Parker, G.. “Flapping Wing Micro Air Vehicle BenchTest Setup” International Journal of Micro Air Vehicles, Vol. 4, No. 1, pp. 51-77, March 2012.
Lynch, A., Batchelor, R., Miller, J., Kiel, B., Gord, J., and Reeder, M. “Spray Characteristics of a Pressure-Swirl Fuel Injector Subjected to a Crossflow and a Coflow,” Atomization and Sprays, Vol. 21, no. 8, pp. 625-643, December 2011.
Reeder, M., Huffman, R., Branam, R., LeBay, K. and Meents, S., “Mixing of a gas-phase buoyant horizontal laminar jet measured with filtered Rayleigh scattering,” Experiments in Fluids, Vol. 50, pp. 1455-1472, June 2011.
Reynolds, T. and Reeder, M., “The Effect of Discrete Blowing Jets on Submerged Inlet Flow Uniformity,” International Journal of Flow Control, Vol. 3, No. 1, pp. 49-66, March 2011.
Reeder, M., Crafton, J., Estevadeordal, J., DeLapp, C.J., McNiel, C., Peltier, D., & Reynolds, T., “Clean seeding for flow visualization and velocimetry measurements,” Experiments in Fluids, Vol. 48, No.5, pp. 889-900, May 2010.
Williams, M., Reeder, M., Maple, R., and Solfelt, D., "Modeling, Simulation, and Flight Tests for a T-38 Talon with Wing Fences,” AIAA Journal of Aircraft, Vol. 47, No. 2, pp. 423-433, March 2010.
Black, J.T., Pitcher, N.A., Reeder, M.F., and R.C. Maple, “Videogrammetry Dynamics Measurements ofa Lightweight Flexible Wing in a Wind Tunnel,” AIAA Journal ofAircraft, Vol. 47, No.1,pp. 172-180, January 2010.
Ol, M., Reeder, M., Fredberg, D., McGowan, G., Gopalarathnam, A., Edwards, J., “Computation vs. Experiment for High-Frequency Low-Reynolds Number Airfoil Plunge,” International Journal of Micro Air Vehicles, Vol. 1, No. 2, pp. 99-119, June 2009.
Gamble, B. & Reeder, M.F., 2009, 'Experimental Analysis of Propeller-Wing Interactions for a Micro Air Vehicle,' AIAA Journal of Aircraft, Vol. 46, No. 1,pp. 65-73, January 2009.
Reeder, M.F., Allen, W., Phillips, M.J., & Dimmick, R.,'Wind Tunnel Measurements of the E- 8C Modeled With and Without Winglets', AIAA Journal of Aircraft, Vo. 45, No. 1, pp. 345-348, January 2008.
Rivera Parga, J., Reeder, M.F., Leveron, T., Blackburn, K.,'An Experimental Study of a Micro Air Vehicle with a Rotatable Tail', AIAA Journal of Aircraft, Vol. 44, No. 6, pp. 1761-1768, November 2007.
Gebbie, D., Reeder, M.F, Tyler, C., Fonov, V., and Crafton, J. 'Lift and Drag Characteristics of a Blended Wing Body Aircraft', AIAA Journal of Aircraft, Vol. 44, No. 5, pp. 1409-1421, September 2007.
DeLuca, A., Reeder, M.F, Freeman, J. and OL, M. 'Flexible- and Rigid-Wing Micro Air Vehicle: Lift and Drag Comparison', AIAA Journal of Aircraft, Vol. 43, No. 2, pp. 572-575, March 2006.
Bjorge, S., Reeder, M., Subramanian, C., Crafton, J. & Fonov, S., 'Flow Around an Object Projected from a Cavity into a Supersonic Freestream,' AIAA Journal, Vol. 43, No. 7, pp. 1465-1476, July 2005.
Heniche, M., Tanguy, P., Reeder, M. & Fasano, J., 'Numerical Investigation of Blade Shape in Static Mixing,' AIChE Journal, Vol. 51, No. 1, pp. 44-58, January 2005.
Subramanian, C., King, P., Reeder, M., Ou, S. & Rivir, R. 'Effects of Strong Irregular Roughness on the Turbulent Boundary Layer,' Flow, Turbulence and Combustion, Vol. 72, pp. 349-368, August 2004.
Pinelli, D., Bakker, A., Myers, K.J., Reeder, M.F., & Fasano, J., Magelli, F, 'Some features of a novel gas dispersion impeller in a dual-impeller configuration', Chemical Engineering Research & Design, Vol. 81, Part A, pp. 448-454, April 2003.
Myers, K., Reeder, M.F. & Ryan, D., 'Power draw of a high-shear homogenizer,' The Canadian Journal of Chemical Engineering, Vol. 79, pp. 94-99, February 2001.
Myers, K., Thomas, A., Bakker, A., Reeder, M., “Performance of a Gas Dispersion Impeller with Vertically Asymmetric Blades,” Chemical Engineering Research and Design (TN), Volume 77, pp. 728-730, November 1999.
Seasholtz, R., Buggele, A., & Reeder, M.F., 'Flow measurements based on Rayleigh scattering and Fabry-Perot interferometer,' Optics and Lasers in Engineering, Vol. 27 (6), pp. 543-570, August 1997.
Reeder, M.F., Samimy, M., & Elliott, G.S., 'An investigation of the effect of tabs on supersonic jets using advanced diagnostics,' AIAA Journal of Propulsion and Power, Vol. 12, No. 4, pp. 742-751, July 1996.
Belovich, V.M., Samimy M. & M.F. Reeder, 1996, 'Dual stream axisymmetric mixing in the presence of axial vorticity,' AIAA Journal of Propulsion and Power, Vol. 12, No. 1, pp. 178-185.
Reeder, M.F. & M. Samimy, 1996, 'The evolution of a jet with vortex-generating tabs: Visualization and analysis of mean and instantaneous properties,' Journal of Fluid Mechanics, Vol. 311, pp. 73-118.
Reeder, M.F. & Zaman, K., 1996, 'Impact of Tab Location Relative to the Nozzle Exit on Jet Distortion,' AIAA Journal (TN), Vol. 34, No. 1, pp. 197-199.
Zaman, K.B., M.F. Reeder, & M. Samimy, 1994, 'Control of an axisymmetric jet using vortex generators,' Physics of Fluids A, Vol. 6 (2), pp. 778-793.
Samimy, M., Zaman, K.B. & Reeder, M.F. 1993, 'Effect of tabs on the flow and noise field of an axisymmetric jet,' AIAA Journal, Vol. 31 (4), pp. 609-619.
Samimy, M., Reeder, M.F., & Elliott, G.S., 1992, 'Compressibility effects on large structures in free shear flows,' Physics of Fluids A, Vol. 4 (6), pp. 1251-1258.
Co-inventor of 4 U.S. patents:
6,059,448, 'An optimized baffle for glass-lined reactors'
6,467,949, 'Static mixer element and method for mixing two fluids'
6,523,995, 'In-tank mixing system and associated radial impeller'
6,883,960, 'Mixing arrangement for tanks'