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

Unsteady force on the flap (nondimensionalised)0.00040.00020.0000-0.0002-0.0004´µÐÔÙÔÔÖ×ÙÖ-0.0006-0.0008-0.0010-4 -3 -2 -1 0 1 2 3 4Flap angle [degrees]Normalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force00 5 10 15 20 25 30 35-0.2-0.4´µÐÔÙÔÔÖ×ÙÖ-0.6-0.8Time (nondimensionalised)-1Unsteady force on the flap (nondimensionalised)0.00060.00040.000200 5 10 15 20 25 30 350.0000-0.2´µÐÔÐÓÛÖ×ÙÖ-0.4-0.0002-0.6-0.0004-0.8Time (nondimensionalised)ÓÖÚÐÙ×ÖØÒÓÒØ­ÔÙÔÔÖÒÐÓÛÖ×ÙÖ׺ÊÆË×ÑÙÐØÓÒØżºÒ ÙÖº½ÌÙÒ×ØÝÓÖÒ­ÔÑÓØÓÒÛÒÚÒ×ÑÐÐÒØÐÔÖØÙÖØÓÒºÍÒ×ØÝ ´µÐÔÐÓÛÖ×ÙÖ-1-4 -3 -2 -1 0 1 2 3 4Flap angle [degrees]ÝÒÑÔÖ××ÙÖ¾ºÈºNormalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force