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Items by Gursul, Ismet

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Number of items: 110.

2014

Hu, T., Wang, Z. and Gursul, I., 2014. Passive control of roll oscillations of low-aspect-ratio wings using bleed. Experiments in Fluids, 55, 1752.

Hu, T., Wang, Z. and Gursul, I., 2014. Attenuation of self-excited roll oscillations of low-aspect-ratio wings by using acoustic forcing. AIAA Journal, 52 (4), pp. 843-854.

Gursul, I., Cleaver, D. J. and Wang, Z., 2014. Forthcoming. Control of low Reynolds number flows by means of fluid–structure interactions. Progress in Aerospace Sciences, 64, pp. 17-55.

Hu, T., Wang, Z. and Gursul, I., 2014. Passive control of self-induced roll oscillations using bleed. In: 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, 2014-01-13 - 2014-01-17.

2013

Calderon, D. E., Wang, Z. and Gursul, I., 2013. Lift-enhancing vortex flows generated by plunging rectangular wings with small amplitude. AIAA Journal, 51 (12), pp. 2953-2964.

Cleaver, D., Wang, Z. and Gursul, I., 2013. Investigation of mechanisms of high lift for a flat-plate airfoil undergoing small-amplitude plunging oscillations. AIAA Journal, 51 (4), pp. 968-980.

Cleaver, D., Calderon, D. E., Wang, Z. and Gursul, I., 2013. Periodically plunging foil near a free surface. Experiments in Fluids, 54 (3), 1491.

Cleaver, D., Wang, Z. and Gursul, I., 2013. Oscillating flexible wings at low Reynolds numbers. In: 51st AIAA Aerospace Sciences Meeting, 2013-01-07 - 2013-01-10, Grapevine, Texas.

Cleaver, D. J., Calderon, D.E., Wang, Z. and Gursul, I., 2013. Low aspect ratio oscillating flexible wings at low Reynolds numbers. In: 43rd AIAA Fluid Dynamics Conference, 2013-06-24 - 2013-06-27, San Diego.

Tregidgo, L., Wang, Z. and Gursul, I., 2013. Unsteady fluid-structure interactions of a pitching membrane wing. Aerospace Science and Technology, 28 (1), pp. 79-90.

Calderon, D.E., Cleaver, D. J., Wang, Z. and Gursul, I., 2013. Wake structure of plunging finite wings. In: 43rd AIAA Fluid Dynamics Conference, 2013-06-24 - 2013-06-27, San Diego.

2012

Tregidgo, L., Wang, Z. and Gursul, I., 2012. Frequency lock-in phenomenon for self-sustained roll oscillations of rectangular wings undergoing a forced periodic pitching motion. Physics of Fluids, 24 (11), 117101.

Wang, Z. and Gursul, I., 2012. Unsteady characteristics of inlet vortices. Experiments in Fluids, 53 (4), pp. 1015-1032.

Calderon, D. E., Wang, Z. and Gursul, I., 2012. Three-dimensional measurements of vortex breakdown. Experiments in Fluids, 53 (1), pp. 293-299.

Calderon, D. E., Wang, Z., Gursul, I. and Visbal, M.R., 2012. Volumetric measurements and simulations of the vortex structures generated by low aspect ratio plunging wings. In: 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Va.: American Institute of Aeronautics and Astronautics.

2011

Rojratsirikul, P., Genc, M. S., Wang, Z. and Gursul, I., 2011. Flow-induced vibrations of low aspect ratio rectangular membrane wings. Journal of Fluids and Structures, 27 (8), pp. 1296-1309.

Cleaver, D. J., Wang, Z., Gursul, I. and Visbal, M. R., 2011. Lift enhancement by means of small-amplitude airfoil oscillations at low Reynolds numbers. AIAA Journal, 49 (9), pp. 2018-2033.

Gresham, N. T., Wang, Z. and Gursul, I., 2011. Effect of slenderness ratio on free-to-roll wing aerodynamics. Journal of Aircraft, 48 (3), pp. 1112-1116.

Wang, Z. and Gursul, I., 2011. An experimental study of the formation and unsteady characteristics of inlet vortices. In: 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, VA.: American Institute of Aeronautics and Astronautics.

Tregidgo, L., Wang, Z. and Gursul, I., 2011. Fluid-structure interactions for a low aspect-ratio membrane wing at low reynolds numbers. In: 41st AIAA Fluid Dynamics Conference and Exhibit 2011, 2011-06-27 - 2011-06-30, Honolulu.

Tregidgo, L., Wang, Z. and Gursul, I., 2011. Low aspect-ratio membrane wing undergoing transient pitching motion at a low Reynolds number. In: 41st AIAA Fluid Dynamics Conference and Exhibit 2011, 2011-06-27 - 2011-06-30, Honolulu.

2010

Gursul, I. and Wang, Z., 2010. High angle of attack aerodynamics. In: Blockley, R. and Shyy, W., eds. Encyclopedia of Aerospace Engineering. Wiley.

Gresham, N. T., Wang, Z. and Gursul, I., 2010. Low Reynolds number aerodynamics of free-to-roll low aspect ratio wings. Experiments in Fluids, 49 (1), pp. 11-25.

Rojratsirikul, P., Wang, Z. and Gursul, I., 2010. Effect of pre-strain and excess length on unsteady fluid-structure interactions of membrane airfoils. Journal of Fluids and Structures, 26 (3), pp. 359-376.

Margaris, P. and Gursul, I., 2010. Vortex topology of wing tip blowing. Aerospace Science and Technology, 14 (3), pp. 143-160.

Jiang, P., Wang, Z. J. and Gursul, I., 2010. Effects of unsteady trailing-edge blowing on delta wing aerodynamics. Journal of Aircraft, 47 (2), pp. 591-602.

Gresham, N., Wang, Z. and Gursul, I., 2010. Vortex dynamics of free-to-roll slender and nonslender delta wings. Journal of Aircraft, 47 (1), pp. 292-302.

Cleaver, D. J., Wang, Z. and Gursul, I., 2010. Vortex mode bifurcation and lift force of a plunging airfoil at low reynolds numbers. In: 48th AIAA Aerospace Sciences Meeting, 2010-01-07 - 2010-01-10, Orlando, Florida.

Calderon, D. E., Wang, Z. and Gursul, I., 2010. Lift enhancement of a rectangular wing undergoing a small amplitude plunging motion. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, VA.: American Institute of Aeronautics and Astronautics.

2009

Gordnier, R. E., Visbal, M. R., Gursul, I. and Wang, Z., 2009. Computational and experimental investigation of a nonslender delta wing. AIAA Journal, 47 (8), pp. 1811-1825.

Cleaver, D., Wang, Z. and Gursul, I., 2009. Lift enhancement on oscillating airfoils. In: 39th AIAA Fluid Dynamics Conference, 2009-06-22 - 2009-06-25, San Antonio, Texas.

Rojratsirikul, P., Wang, Z. and Gursul, I., 2009. Unsteady fluid-structure interactions of membrane airfoils at low Reynolds numbers. Experiments in Fluids, 46 (5), pp. 859-872.

Gresham, N., Wang, Z. and Gursul, I., 2009. Aerodynamics of Free-to-Roll Low Aspect Ratio Wings. In: 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, Florida.

Cleaver, D., Wang, Z. and Gursul, I., 2009. Delay of stall by small amplitude airfoil oscillation at low reynolds numbers. In: 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, Florida.

Rojratsirikul, P., Wang, Z. and Gursul, I., 2009. Effect of Pre-Strain and Excess Length on Unsteady Fluid-Structure Interactions of Membrane Airfoils. In: 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, Florida.

Gresham, N. T., Wang, Z. J. and Gursul, I., 2009. Self-induced roll oscillations of nonslender wings. AIAA Journal, 47 (3), pp. 481-483.

2008

Williams, N., Wang, Z. and Gursul, I., 2008. Active flow control on a nonslender delta wing. Journal of Aircraft, 45 (6), pp. 2100-2110.

Vardaki, E., Wang, Z. and Gursul, I., 2008. Flow reattachment and vortex re-formation on oscillating low-aspect-ratio wings. AIAA Journal, 46 (6), pp. 1453-1462.

Marles, D., Margaris, P. and Gursul, I., 2008. Effect of an Axial Jet on Aircraft Wake Vortices. In: International Workshop on Fundamental Issues Related to Aircraft Trailing Wakes, 2008-05-27 - 2008-05-29, Marseille.

Marles, D. and Gursul, I., 2008. Effect of an axial jet on vortex merging. Physics of Fluids, 20 (4), 047101.

Heathcote, S., Wang, Z. and Gursul, I., 2008. Effect of spanwise flexibility on flapping wing propulsion. Journal of Fluids and Structures, 24 (2), pp. 183-199.

Margaris, P., Marles, D. and Gursul, I., 2008. Experiments on Jet/Vortex Interaction. Experiments in Fluids, 44 (2), pp. 261-278.

Williams, N., Wang, Z. and Gursul, I., 2008. Active Flow Control on a Nonslender Delta Wing. In: AIAA 46th Aerospace Sciences Meeting, 2008-01-07 - 2008-01-10, Reno NV.

Rojratsirikul, P., Wang, Z. and Gursul, I., 2008. Unsteady Aerodynamics of Membrane Airfoils. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, Nevada.

Gursul, I., 2008. Fluid-Structure Interaction Research at the University of Bath. In: AFOSR Workshop on Aeroelasticity, Unsteady Aerodynamics, and Fluid-Structure Interaction, 2008-02-11 - 2008-02-12, Arlington, VA.

Gresham, N. T., Wang, Z. J. and Gursul, I., 2008. Vortex Dynamics of Delta Wings Undergoing Self-Excited Roll Oscillations. In: 38th AIAA Fluid Dynamics Conference and Exhibit, 2008-06-23 - 2008-06-26, Reno NV.

2007

Gursul, I., Wang, Z. and Vardaki, E., 2007. Review of Flow Control Mechanisms of Leading-edge Vortices. Progress in Aerospace Sciences, 43 (7-8), pp. 246-270.

Gursul, I., 2007. Self-Excited Roll Oscillations of Nonslender Wings. In: AFOSR Contractors Meeting, 2007-08-01, Long Beach.

Gordnier, R. E., Visbal, M. R., Gursul, I. and Wang, Z., 2007. Computational and Experimental Investigation of a Nonslender Delta Wing. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007-01-01, Reno, Nevada.

Gursul, I., Vardaki, E., Margaris, P. and Wang, Z., 2007. Control of wing vortices. In: Active flow control. Germany: Springer, pp. 137-151.

Marles, D. and Gursul, I., 2007. Effect of a jet on vortex merging. In: 37th AIAA Fluid Dynamics Conference, 2007-01-01, Miami, FL.

Wang, Z., Jiang, P. and Gursul, I., 2007. Effect of thrust vectoring jets on delta wing aerodynamics. Journal of Aircraft, 44 (6), pp. 1877-1888.

Margaris, P., Marles, D. and Gursul, I., 2007. Experiments on interaction of a jet with a trailing vortex. In: 45th AIAA Aerospace Sciences Meeting, 2007-01-01, Reno, NV.

Heathcote, S. and Gursul, I., 2007. Flexible flapping airfoil propulsion at low reynolds numbers. AIAA Journal, 45 (5), pp. 1066-1079.

Heathcote, S. and Gursul, I., 2007. Jet switching phenomenon for a periodically plunging airfoil. Physics of Fluids, 19 (2), 027104.

Taylor, G., Wang, Z., Vardaki, E. and Gursul, I., 2007. Lift enhancement over flexible nonslender delta wings. AIAA Journal, 45 (12), pp. 2979-2993.

McClain, A., Wang, Z., Vaidaki, E. and Gursul, I., 2007. Unsteady aerodynamics of free-to-roll nonslender delta wings. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007-01-01, Reno, Nevada.

Gursul, I., 2007. Vortex Flows of Unmanned Air Vehicles. In: AIAC-2007-003, Ankara International Aerospace Conference, 2007-09-10 - 2007-09-12, METU Ankara.

Margaris, P. and Gursul, I., 2007. Vortex topology of wing tip blowing. In: 45th AIAA Aerospace Sciences Meeting, 2007-01-01, Reno, NV.

2006

Gursul, I., Vardaki, E., Margaris, P. and Wang, Z., 2006. Control of Wing Vortices. In: Conference on Active Flow Control, 2006-09-01, Berlin.

Gursul, I., Vardaki, E. and Wang, Z., 2006. Active and passive control of reattachment on various low-sweep wings. In: 44th AIAA Aerospace Sciences Meeting, 2006-01-01, Reno, NV.

Heathcote, S., Wang, Z. and Gursul, I., 2006. Effect of spanwise flexibility on flapping wing propulsion. In: 36th AIAA Fluid Dynamics Conference, 2006-01-01, San Francisco, CA.

Whitehead, J. and Gursul, I., 2006. Interaction of synthetic jet propulsion with airfoil aerodynamics at low Reynolds numbers. AIAA Journal, 44 (8), pp. 1753-1766.

Gursul, I., Wang, Z. and Vardaki, E., 2006. Review of flow control mechanisms of leading-edge vortices. In: 36th AIAA Fluid Dynamics Conference and Exhibit, 2006-01-01, San Francisco, California.

Lynn, R. J. and Gursul, I., 2006. Vortex dynamics on a generic UCAV configuration. In: 44th AIAA Aerospace Sciences Meeting, 2006-01-01, Reno, NV.

Margaris, P. and Gursul, I., 2006. Wing tip vortex control using synthetic jets. Aeronautical Journal, 110 (1112), pp. 673-681.

2005

Wang, Z. and Gursul, I., 2005. Effects of Jet/Vortex Interaction on Delta Wing Aerodynamics. In: 1st International Conference on Innovation and Integration in Aerospace Sciences, 2005-08-01, Queen's University, Belfast, Northern Ireland.

Margaris, P. and Gursul, I., 2005. Wing Tip Vortex Control Using Synthetic Jets. In: CEAS/KATnet Conference on Key Aerodynamic Technologies, 2005-06-01, Bremen.

Gursul, I., 2005. Propulsion Related Vortical Flow Issues for Unmanned Air Vehicles. In: Propulsion Systems for Unmanned Aircraft, Institution of Mechanical Engineers, 2005-04-01, Bristol.

Heathcote, S. and Gursul, I., 2005. Flexible flapping airfoil propulsion at low Reynolds numbers. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005-01-01, Reno, NV.

Gursul, I., Allan, M. R. and Badcock, K. J., 2005. Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics. Aerospace Science and Technology, 9 (3), pp. 181-189.

Taylor, G., Kroker, A. and Gursul, I., 2005. Passive flow control over flexible non-slender delta wings. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005-01-01, Reno, NV.

Vardaki, E., Gursul, I. and Taylor, G. S., 2005. Physical mechanisms of lift enhancement for flexible delta wings. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005-01-01, Reno, NV.

Gursul, I., 2005. Review of unsteady vortex flows over slender delta wings. Journal of Aircraft, 42 (2), pp. 299-319.

Taylor, G. S. and Gursul, I., 2005. Support interference for a maneuvering delta wing. Journal of Aircraft, 42 Nov-Dec (6), pp. 1504-1515.

Gursul, I., Gordnier, R. and Visbal, M., 2005. Unsteady Aerodynamics of Nonslender Delta Wings. Progress in Aerospace Sciences, 41 (7), pp. 515-557.

2004

Margaris, P. and Gursul, I., 2004. Effect of Steady Blowing on Wing Tip Flowfield. In: 2nd AIAA Flow Control Conference, 2004-06-01, Portland.

Heathcote, S. and Gursul, I., 2004. Jet switching phenomenon for a plunging airfoil. In: 34th AIAA Fluid Dynamics Conference and Exhibit, 2004-06-01, Portland.

Taylor, G. S. and Gursul, I., 2004. Lift Enhancement over a Flexible Delta Wing. In: 2nd AIAA Flow Control Conference, 2004-06-01, Portland.

Gursul, I., 2004. Vortex Flows on UAVs: Issues and Challenges. In: 42nd Aeropsace Sciences Meeting and Exhibit, 2004-01-01, Reno, Nevada.

Taylor, G. S. and Gursul, I., 2004. Buffeting flows over a low-sweep delta wing. AIAA Journal, 42 (9), pp. 1737-1745.

Lambert, C. and Gursul, I., 2004. Characteristics of fin buffeting over delta wings. Journal of Fluids and Structures, 18 (SUPPL), pp. 307-319.

Heathcote, S., Martin, D. and Gursul, I., 2004. Flexible flapping airfoil propulsion at zero freestream velocity. AIAA Journal, 42 (11), pp. 2196-2204.

Whitehead, J. A. and Gursul, I., 2004. Interaction of synthetic JET propulsion with wing aerodynamics at low reynolds numbers.

Gursul, I., 2004. Recent developments in delta wing aerodynamics. Aeronautical Journal, 108 (1087), pp. 437-452.

Taylor, G. S. and Gursul, I., 2004. Unsteady vortex flows and buffeting of a low sweep delta wing. In: AIAA, 2004-01-01, Reno, NV.

Gursul, I., 2004. Vortex flows on UAVs: Issues and challenges. Aeronautical Journal, 108 (1090), pp. 597-610.

Vardaki, E. and Gursul, I., 2004. Vortex flows on a rolling nonslender delta wing. In: 22nd AIAA Applied Aerodynamics Conference, 2004-01-01, Providence, RI.

2003

Gursul, I. and Allan, M., 2003. Delta Wing Aerodynamics : Requirements from CFD and Experiments. In: Integrating CFD and Experiments in Aerodynamics, 2003-09-01, Glasgow.

Whitehead, J. and Gursul, I., 2003. Aerodynamics and Propulsion of Synthetic Jet Based Micro Air Vehicles. In: AIAA Fluid Dynamics Conference, 2003-06-01, Orlando, FL.

Taylor, G. S., Schnorbus, T. and Gursul, I., 2003. An Investigation of Vortex Flows over Low Sweep Delta Wings. In: AIAA Fluid Dynamics Conference, 2003-06-01, Orlando, FL.

Lambert, C. and Gursul, I., 2003. Fin Buffeting over Various Delta Wings. In: AIAA Applied Aerodynamics Conference, 2003-06-01, Orlando, FL.

Heathcote, S. F. and Gursul, I., 2003. Flexible Flapping Wing Propulsion at Zero Freestream Velocity. In: AIAA Fluid Dynamics Conference, 2003-06-01, Orlando, FL.

Gursul, I., 2003. Review of Unsteady Vortex Flows over Delta Wings. In: AIAA Applied Aerodynamics Conference, 2003-06-01, Orlando, FL.

Gray, J., Gursul, I. and Butler, R., 2003. Aeroelastic Response of a Flexible Delta Wing Due to Unsteady Vortex Flows. In: 41st Aerospace Sciences Meeting and Exhibit, 2003-01-01, Reno, NV.

Taylor, G., Gursul, I. and Greenwell, D., 2003. An Investigation of Support Interference in High Angle of Attack Testing. In: 41st Aerospace Sciences Meeting and Exhibit, 2003-01-01, Reno, NV.

Lee, Y. L. and Gursul, I., 2003. An Investigation of Unsteady Interactions of a Vortex Pair over Delta Wings. In: 41st Aerospace Sciences Meeting and Exhibit, 2003-01-01, Reno, NV.

Phillips, S., Lambert, C. and Gursul, I., 2003. Effect of a trailing-edge jet on fin buffeting. Journal of Aircraft, 40 (3), pp. 590-599.

Gursul, I., 2003. Flow-Structure Interaction on Flexible UCAV Wings. In: Air Force Office of Scientific Research 2003 Contractors' Meeting in Unsteady Aerodynamics and Hypersonics, 2003-09-10 - 2003-09-12, Destin, Florida.

Taylor, G. S., Gursul, I. and Greenwell, D. I., 2003. Investigation of support interference in high-angle-of-attack testing. Journal of Aircraft, 40 (1), pp. 143-152.

Wooding, C. L. and Gursul, I., 2003. Unsteady Aerodynamics of Low Aspect Ratio Wings at Low Reynolds Numbers. In: Royal Aeronautical Society Aerospace Aerodynamics Research Conference, 2003-06-10 - 2003-06-12, London.

Gursul, I., 2003. Unsteady Aspects of Leading-Edge Vortices. Working Paper. NATO.

2002

Gursul, I., 2002. Vortex Flows on UAVs: Issues and Challenges. In: Workshop on Aerodynamic Issues of Unmanned Air Vehicles, 2002-11-01, University of Bath.

Gursul, I., Taylor, G. and Wooding, C. L., 2002. Vortex Flows over Fixed-Wing Micro Air Vehicles. In: 40th AIAA Aerospace Meeting and Exhibit, 2002-01-01, Reno, NV.

Phillips, S., Lambert, C. and Gursul, I., 2002. Effect of a Trailing-Edge Jet on Fin Buffeting. In: 1st AIAA Flow Control Conference, 2002-06-24 - 2002-06-26, St. Louis, Missouri.

2001

Lambert, C. and Gursul, I., 2001. Buffeting of a Flexible Fin Over a Delta Wing. In: 19th AIAA Applied Aerodynamics Conference, 2001-06-01, Anaheim.

Taylor, G., Gursul, I. and Greenwell, D., 2001. Static Hysteresis of Vortex Breakdown Due to Support Interference. In: 19th AIAA Applied Aerodynamics Conference, 2001-06-01, Anaheim.

Gursul, I. and Xie, W., 2001. Interaction of vortex breakdown with an oscillating fin. AIAA Journal, 39 (3), pp. 438-446.

Taylor, G. S., Gursul, I. and Greenwell, D. I., 2001. Static hysteresis of vortex breakdown due to support interference. In: 19th AIAA Applied Aerodynamics Conference, 2001. Reston, Canada: American Institute of Aeronautics and Astronautics.

2000

Gursul, I., 2000. A proposed mechanism for the time lag of vortex breakdown location in unsteady flows. In: 38th Aerospace Sciences Meeting and Exhibit, 2000, 2000-01-10 - 2000-01-13, Reno.

This list was generated on Thu Oct 2 13:26:58 2014 IST.