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

20152010Flap angle [degrees]50-5-10-15Flap angle [degreees]100-10-200 1 2 3 4 5 6 7Nondimensionalised time-200 1 2 3 4 5 6Nondimensionalised time´µÊÝÒÓÐ×ÒÙÑÖ¿ÑÐÐÓÒFlap hingeÙÖº½ËÓÐÓØÓÒ×ÓÖ××Øżº¸ÊÆË×ÑÙÐØÓÒº ´µÊÝÒÓÐ×ÒÙÑÖ¾½ÑÐÐÓÒFlap hingeP: 0.6 0.632653 0.665306 0.697959 0.730612 0.763265 0.795918P: 0.6 0.632653 0.665306 0.697959 0.730612 0.763265 0.795918P: 0.35 0.39 0.43 0.47 0.51 0.55 0.59 0.63 0.67 0.71 0.75 0.79 0.83 0.87 0.91 0.95P: 0.35 0.39 0.43 0.47 0.51 0.55 0.59 0.63 0.67 0.71 0.75 0.79 0.83 0.87 0.91 0.95ÙÖº½ËÔÖØÓÒÓÒØ­ÔÐÓÒÙÞÞÝкÁÒ×ØÒØÒÓÙ×­ÔÒÐÓ½¼¿Æ¸ÊÆË ×ÑÙÐØÓÒº ´µÊÝÒÓÐ×ÒÙÑÖ¿ÑÐÐÓÒ ´µÊÝÒÓÐ×ÒÙÑÖ¾½ÑÐÐÓÒ18Mach 0.98, Euler equations, dynamic pressure 26.486 kPaEuler25Mach 0.987, RANS equations, dynamic pressure 26.468 kPaRANS16142012Flap angle [degrees]151081064ÙÖº¾¼«ØÓÑÔÒÓÒÙÞÞÑÔÐØÙ ´µ5201 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24½¼¼251 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25Percentage dampingPercentage damping´µ0Flap angle [degrees]