Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

B-F-R Case, Euler Simulation, Mach 1.05´µÌ¹¹Ê×ØŽº¼P: 0.420 0.477 0.522 0.567 0.612 0.659 0.704 0.750 0.797 0.841 0.890B-F-R-T Case, Euler Simulations, Mach 1.05´µÌ¹¹Ê¹Ì×ØŽº¼P: 0.4330 0.5041 0.5600 0.6158 0.6700 0.7275 0.7800 0.8392 0.8900B-F-W-R-T Case, Euler Simulation, Mach 1.05ÙÖº¿¿ÀÛ×ØÝÔÖ××ÙÖÓÒØÓÙÖ×ØŽº¼ÓÖÒÖ×ÒÐÚÐÓÓÑØÖ ÓÑÔÐÜØÝ×ÓÛÒØÖÙÐÓÖÑØÓÒÓ×ÓÓجҺ××´µÒ´µÛØÓÙØ ´µÌ¹¹Ï¹Ê¹Ì×ØŽº¼P: 0.433 0.484 0.524 0.565 0.606 0.646 0.687 0.728 0.768 0.809 0.849 0.890ØÛÒ×ÓÛ×ÓÓÚÖØÖÙÖº ½¿