论文信息 - Effect of Pitch-Up Motion on Flow Structure Adjacent to the X-45 Planform - 字舞流文

Effect of Pitch-Up Motion on Flow Structure Adjacent to the X-45 Planform

M. Elkhoury | M. Elkhoury

[1] Lars E. Ericsson. Vortex Characteristics of Pitching Double-Delta Wings , 1999 .

[2] M. Elkhoury,et al. Visualized vortices on unmanned combat air vehicle planform: Effect of Reynolds number , 2004 .

[3] S. M. Batill,et al. Vortex Dynamics on a Pitching Delta Wing , 1990 .

[4] Russell M. Cummings,et al. Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation , 2012 .

[5] Russell M. Cummings,et al. Numerical Prediction and Wind Tunnel Experiment for a Pitching Unmanned Combat Air Vehicle , 2008 .

[6] Ismet Gursul,et al. An Investigation of Vortex Flows over Low Sweep Delta Wings , 2003 .

[7] Donald Rockwell,et al. Flow structure on finite-span wings due to pitch-up motion , 2011, Journal of Fluid Mechanics.

[9] Miguel R. Visbal,et al. Unsteady aerodynamics of nonslender delta wings , 2005 .

[10] D. Rockwell,et al. Near-Surface Topology of Unmanned Combat Air Vehicle Planform: Reynolds Number Dependence , 2005 .

[11] Neal T. Frink,et al. Three Unstructured Computational Fluid Dynamics Studies on Generic Unmanned Combat Aerial Vehicle , 2012 .