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

0.010.008Mach 0.95, Euler equations, dynamic pressure 5.4 kPaWing impulseFlap impulse0.040.03Mach 0.95, Euler equations, dynamic pressure 5.4 kPaWing impulseFlap impulse0.0060.0040.020.002Generalised coordinate0-0.002-0.004-0.006-0.008´µÅÓ½-0.040.01-0.010 50 100 150 200Non-dimensionalised timeGeneralised coordinate0-0.01-0.02-0.03´µÅÓ¾0 50 100 150 200Non-dimensionalised time0.00040.0003Mach 0.95, Euler equations, dynamic pressure 5.4 kPaWing impulseFlap impulse0.0010.0008Mach 0.95, Euler equations, dynamic pressure 5.4 kPaWing impulseFlap impulse0.00020.00060.0004Generalised coordinate1e-040-0.0001-0.0002-0.0003´µÅÓ¿-0.001-0.00040 50 100 150 200Non-dimensionalised timeGeneralised coordinate0.00020-0.0002-0.0004-0.0006-0.0008´µÅÓ0 50 100 150 200Non-dimensionalised time8e-056e-05Mach 0.95, Euler equations, dynamic pressure 5.4 kPaWing impulseFlap impulse0.020.015Mode 1Mode 2Mode 3Mode 4Mode 5Mach 1.05, Euler equations, wing impulse, dynamic pressure 5.4 kPa4e-050.012e-05Generalised coordinate0´µÅÓ-0.020.005-2e-05-0.005-4e-05-0.01ÙÖº¾¾ÓÑÒØÓÒÓ×ÓÒÙÖÓÐ×ØÖ×ÔÓÒ×ØÖØÖÒ×ÓÒÅÒÙÑÖ×-6e-05-0.015-8e-050 50 100 150 2000 50 100 150 200Non-dimensionalised timeNon-dimensionalised time½¼¿Generalised coordinate´µÅÓÐÖ×ÔÓÒ×ÓÐÐÑÓ×ØŽº¼0