Bio
Hometown: Reno, Nevada
Officer, United States Air Force (2000-2008)
Senior Multi-disciplined Engineer, Raytheon Missile Systems (2004-2008)
Senior Lecturer, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia (2008-Present)
Education
B.S. Mechanical Engineering – University of California, San Diego
M.S. Aeronautics and Astronautics – Stanford University
Ph.D. Aeronautical Engineering – University of New South Wales
Research and Scholarly Interests
Low Reynolds Number Flapping Wing Aerodynamics
Hypersonic Fluid Structure Interaction
Publications
JOURNAL PUBLICATIONS
“Enhancing the Power-Extraction Efficiency of a Flapping Foil via Active Morphing”, C. M. Hoke, J. Young, J.C.S. Lai, AIAA Journal (Under Review)
“Effects of Time-varying Camber Deformation on Flapping Foil Propulsion and Power Extraction”, C. M. Hoke, J. Young, J. C. S. Lai, Journal of Fluids and Structures Vol. 56 (2015)
“Thermal Analysis of Hypersonic Inlet Flow with Exergy-Based Design Methods”, David J. Moorhouse and Charles M. Hoke, International Journal of Applied Thermodynamics, Vol. 5 (No. 4), pp. 161-166, December 2002, ISSN 1302-9724
“Investigation of Oscillating Foil Power Generation in Constrained Flow”, Hoke, C. M., Young, J., Lai, J. C. S., Karakas, F., Zaloglu, B., & Fenercioglu, I. (2017). Procedia Engineering, 199, 3450-3455.
PROFESSIONAL PRESENTATIONS
F. Karakas, B. Zaloglu, I. Fenercioglu, C. Hoke, J. Young, J. Lai, M. F. Platzer, “On Optimal Oscillating-Foil Power Generation in Free and Constrained Flow”, AIAA SciTech Forum, American Institute of Aeronautics and Astronautics, 2016.
Hoke, C., Young, J., Lai, J.C.S., “Time-varying Flexible Airfoil Shape Effects on Flapping Airfoil Power Extraction.” 52nd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, National Harbor, Maryland 2014.
“High Resolution Simulation of Full Aircraft Control at Flight Reynolds Numbers”, Charles M. Hoke, Stephen L. Greenwade, 2007 AIAA Region V SPC, United States Air Force Academy, Colorado, Apr. 10-12, 2007
“Validation and Prediction of the C130P Combat shadow using CFD”, Charles M. Hoke, Andrew Teigeler, 2007 AIAA Region V SPC, United States Air Force Academy, Colorado, Apr. 10-12, 2007
“Aerodynamic Analysis of Complex Missile Configurations Using AVUS (Air Vehicles Unstructured Solver) “, Charles M. Hoke, Victor Burnley, Gregory Schwabacher, 22nd Applied Aerodynamics Conference and Exhibit, Providence, Rhode Island, Aug. 16-19, 2004
“Exergy Effect on the Hypersonic Vehicle Design Space”, Charles M. Hoke, 11th AIAA/AAAF International Conference Orleans, France, 29 September – 04 October, 2002