Osama A. Kandil
Affiliations: | Old Dominion University, Norfolk, VA, United States |
Area:
Aerospace Engineering, Fluid and Plasma Physics, Applied MechanicsGoogle:
"Osama Kandil"Mean distance: (not calculated yet)
Children
Sign in to add traineeJuan A. Pelaez | grad student | 2003 | Old Dominion University |
Hongwu Zhao | grad student | 2003 | Old Dominion University |
Nitin Khasdeo | grad student | 2007 | Old Dominion University |
Kursat Kara | grad student | 2008 | Old Dominion University |
Isik A. Ozcer | grad student | 2009 | Old Dominion University |
Bedri Yagiz | grad student | 2010 | Old Dominion University |
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Publications
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Elmekawy A, Kandil OA, Baysal O. (2014) F/A-18 twin-tail buffet modeling using non-linear eddy viscosity models 44th Aiaa Fluid Dynamics Conference |
Yagiz B, Kandil O, Pehlivanoglu YV. (2012) Drag minimization using active and passive flow control techniques Aerospace Science and Technology. 17: 21-31 |
Kara K, Balakumar P, Kandil OA. (2011) Effects of Nose Bluntness on Hypersonic Boundary-Layer Receptivity and Stability over Cones Aiaa Journal. 49: 2593-2606 |
Pehlivanoglu YV, Yagiz B, Kandil O, et al. (2010) Particle swarm optimization of suction and blowing on airfoils at transonic speeds Journal of Aircraft. 47: 1955-1965 |
Hill GA, Kandil OA, Hahn AS. (2007) Aerodynamic Investigations of an Advanced Over-the-Wing Nacelle Transport Aircraft Configuration Journal of Aircraft. 46: 25-35 |
Sheta EF, Kandil OA. (2002) Effect Of Dynamic Rolling Oscillations On Twin-Tail Buffet Response Journal of Sound and Vibration. 252: 261-280 |
Sheta EF, Kandil OA, Yang Z. (1998) Effectiveness Of Flow Control For Alleviation Of Twin-Tail Buffet Sae Transactions. 107: 1421-1431 |
Kandil OA, Sheta EF. (1998) Coupled and Uncoupled Bending-Torsion Responses of Twin-Tail Buffet Journal of Fluids and Structures. 12: 677-701 |
Kandil OA, Massey SJ, Sheta EF. (1996) Structural Dynamic/CFD Interaction for Computation of Vertical Tail Buffet Aeronautical Journal. 100: 297-303 |
Hu H, Kandil OA. (1994) A Hybrid Boundary Element-Finite Volume Method for Unsteady Transonic Airfoil Flows Engineering Analysis With Boundary Elements. 14: 149-157 |