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Osama A. Kandil - Publications

Affiliations: 
Old Dominion University, Norfolk, VA, United States 
Area:
Aerospace Engineering, Fluid and Plasma Physics, Applied Mechanics
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28 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2014 Elmekawy A, Kandil OA, Baysal O. F/A-18 twin-tail buffet modeling using non-linear eddy viscosity models 44th Aiaa Fluid Dynamics Conference. DOI: 10.2514/1.C033482  0.404
2012 Yagiz B, Kandil O, Pehlivanoglu YV. Drag minimization using active and passive flow control techniques Aerospace Science and Technology. 17: 21-31. DOI: 10.1016/J.Ast.2011.03.003  0.646
2011 Kara K, Balakumar P, Kandil OA. Effects of Nose Bluntness on Hypersonic Boundary-Layer Receptivity and Stability over Cones Aiaa Journal. 49: 2593-2606. DOI: 10.2514/1.J050032  0.679
2010 Pehlivanoglu YV, Yagiz B, Kandil O, Baysal O. Particle swarm optimization of suction and blowing on airfoils at transonic speeds Journal of Aircraft. 47: 1955-1965. DOI: 10.2514/1.C000233  0.652
2007 Hill GA, Kandil OA, Hahn AS. Aerodynamic Investigations of an Advanced Over-the-Wing Nacelle Transport Aircraft Configuration Journal of Aircraft. 46: 25-35. DOI: 10.2514/1.39730  0.487
2002 Sheta EF, Kandil OA. Effect Of Dynamic Rolling Oscillations On Twin-Tail Buffet Response Journal of Sound and Vibration. 252: 261-280. DOI: 10.1006/Jsvi.2001.3877  0.36
1998 Sheta EF, Kandil OA, Yang Z. Effectiveness Of Flow Control For Alleviation Of Twin-Tail Buffet Sae Transactions. 107: 1421-1431. DOI: 10.4271/985501  0.579
1998 Kandil OA, Sheta EF. Coupled and Uncoupled Bending-Torsion Responses of Twin-Tail Buffet Journal of Fluids and Structures. 12: 677-701. DOI: 10.1006/Jfls.1998.0168  0.508
1996 Kandil OA, Massey SJ, Sheta EF. Structural Dynamic/CFD Interaction for Computation of Vertical Tail Buffet Aeronautical Journal. 100: 297-303. DOI: 10.1017/S0001924000028943  0.515
1994 Hu H, Kandil OA. A Hybrid Boundary Element-Finite Volume Method for Unsteady Transonic Airfoil Flows Engineering Analysis With Boundary Elements. 14: 149-157. DOI: 10.1016/0955-7997(94)90091-4  0.464
1992 Liu CH, Kandil OA, Wong T. Passive control of supersonic asymmetric vortical flows around cones Impact of Computing in Science and Engineering. 4: 80-96. DOI: 10.1016/0899-8248(92)90017-3  0.611
1992 Kandil OA, Wong T, Liu CH. Numerical simulation of steady and unsteady asymmetric vortical flow Journal of Fluids and Structures. 6: 249-265. DOI: 10.1016/0889-9746(92)90047-7  0.622
1992 Liu CH, Wong T, Kandil OA. Prediction of asymmetric vortical flows around slender bodies using Navier-Stokes equations Fluid Dynamics Research. 10: 409-450. DOI: 10.1016/0169-5983(92)90032-R  0.615
1991 Kandil OA, Wong T, Liu CH. Prediction of steady and unsteady asymmetric vortical flows around circular cones Aiaa Journal. 29: 2169-2178. DOI: 10.2514/3.10855  0.59
1991 Kandil OA, Kandil HA. Computation of compressible quasi-axisymmetric slender vortex flow and breakdown Computer Physics Communications. 65: 164-172. DOI: 10.1016/0010-4655(91)90169-L  0.542
1990 Kandil OA, Hu H. Integral solution of unsteady full-potential equation for a transonic pitching airfoil Journal of Aircraft. 27: 123-130. DOI: 10.2514/3.45907  0.459
1990 Kandil OA, Chuang HA. Unsteady inviscid and viscous computations for vortex-dominated flows Journal of Aircraft. 27: 387-388. DOI: 10.2514/3.25287  0.596
1990 Kandil OA, Chuang HA. Computation of vortex-dominated flow for a delta wing undergoing pitching oscillation Aiaa Journal. 28: 1589-1595. DOI: 10.2514/3.25257  0.607
1989 Kandil OA, Chuang HA. Unsteady Navier-Stokes computations past oscillating delta wing at high incidence Aiaa Journal. 28: 1565-1572. DOI: 10.2514/3.25254  0.606
1989 Kandil OA, Chuang HA. Unsteady Transonic Airfoil Computation Using Implicit Euler Scheme on Body-Fixed Grid Aiaa Journal. 27: 1031-1037. DOI: 10.2514/3.10217  0.612
1989 Eslami H, Kandil OA. Nonlinear forced vibration of orthotropic rectangular plates using the method of multiple scales Aiaa Journal. 27: 955-960. DOI: 10.2514/3.10204  0.331
1988 Kandil OA, Chuang HA. Computation of steady and unsteady vortex-dominated flows with shock waves Aiaa Journal. 26: 524-531. DOI: 10.2514/3.9929  0.589
1988 Liu CH, Wong TC, Kandil OA. Separation-bubble flow solution using Euler/Navier-Stokes zonal approach with downstream compatibility conditions Journal of Scientific Computing. 3: 121-137. DOI: 10.1007/Bf01061253  0.524
1987 Kandil OA, Chuang AH. Influence of numerical dissipation on computational Euler equations for vortex-dominated flows Aiaa Journal. 25: 1426-1434. DOI: 10.2514/3.9800  0.51
1987 Kandil OA, Hu H. Full-potential integral solution for transonic flows with and without embedded Euler domains Aiaa Journal. 26: 1079-1086. DOI: 10.2514/3.10014  0.515
1986 Kandil OA, Yates EC. Transonic Vortex Flows Past Delta Wings: Integral Equation Approach Aiaa Journal. 24: 1729-1736. DOI: 10.2514/3.9517  0.456
1985 Kandil OA. Computational technique for compressible vortex flows past wings at large incidence Journal of Aircraft. 22: 750-755. DOI: 10.2514/3.45197  0.553
1984 Kandil OA, Chu L, Tureaud T. A Nonlinear Hybrid Vortex Method for Wings at Large Angle of Attack Aiaa Journal. 22: 329-336. DOI: 10.2514/3.8396  0.483
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