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1274 PATEL ET AL. [23] Visser, K. D., and Nelson, R. C., “Measurements of Circulation and Vorticity in the Leading-Edge Vortex of a Delta Wing,” AIAA Journal, Vol. 31, No. 1, Jan. 1993, pp. 104–111. [24] Visser, K. D., Ferrero, M., and Nelson, R. C., “Physical Considerations of Leading-Edge Flows,” AIAA Paper 2004-5083, Aug. 2004. [25] Moeller, E. B., and Rediniotis, O. K., “Hingeless Flow Control over a Delta Wing Platform,” AIAA Paper 2000-117, Jan. 2000. [26] Amitay, M., Washburn, A. E., Anders, S. G., and Parekh, D., “Active Flow Control on the Stingray Uninhabited Air Vehicle: Transient Behavior,” AIAA Journal, Vol. 42, No. 11, Nov. 2004, pp. 2205–2215. [27] Visser, K. D., “An Investigation of the Effects of an External Jet on the Performance of a Highly Swept Delta Wing,” M.S. Thesis, Univ. of Notre Dame, Notre Dame, IN, 1988. [28] Visser, K. D., Nelson, R. C., and Ng, T. T., “A Flow Visualization and Force Data Evaluation of Spanwise Blowing on Full and Half Span Delta Wings,” AIAA Paper 89-0192, Jan. 1989. [29] Visser, K. D., Iwanski, K. P., Nelson, R. C., and Ng, T. T., “Control of Leading Edge Vortex Breakdown by Blowing,” AIAA Paper 88-0504, Jan., 1988. [30] Zhang, F., Khalid, M., and Ball, N., “A CFD Based Study of UCAV 1303 Model,” AIAA Paper 2005-5615, June 2005. [31] Nelson, R., Corke, T. C., He, C., Otham, H., Matsumo, T., Patel, M. P., and Ng, T. T., “Modification of the Flow Structure over a UAV Wing for Roll Control,” AIAA Paper 2007-884, Jan. 2007. [32] Lopera, J., Ng, T. T., Patel, M. P., Vasudevan, S., and Corke, T. C., “Aerodynamic Control of 1303 UAV Using Windward Plasma Actuators on a Separation Ramp,” AIAA Paper 2007-0636, Jan. 2007. [33] Wong, M., McKenzie, G., Ol, M., Petterson, K., Zhang, S., “Joint TTCP CFD Studies into the 1303 UCAV Performance: First Year Results,” AIAA Paper 2006-2984, June 2006. [34] S. McParlin, S., Bruce, R., Hepworth, A., and Rae, A., “Low Speed Wind Tunnel Tests on the 1303 UCAV Concept,” AIAA Paper 2006- 2985, June 2006. [35] Petterson, K., “Low-Speed Aerodynamic and Flowfield Characteristics of a UCAV,” AIAA Paper 2006-2986, June 2006. [36] Wong, M., and Flores, J., “Application of OVERFLOW-MLP to the Analysis of the 1303 UCAV,” AIAA Paper 2006-2987, June 2006. [37] Milne, M., and Arthur, M., “Evaluation of Bespoke and Commercial CFD Methods for a UCAV Configuration,” AIAA Paper 2006-2988, June 2006. View publication statsPDF Image | Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle
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