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

P: 0.6 0.666667 0.733333 0.8 0.866667 0.933333 1ÙÖº¾¼ËØÝÒÚ×ÔÖ××ÙÖÓÒØÓÙÖ×ÓÖØËËÌ׿ºÌÖÓÒÓÐÓÛÔÖ××ÙÖ ØØ­ÔÐÒ××ÙÔÖ×ÓÒ­ÓÛº ´µËÙÖÔÓÒØÓÙÖ׺ ´µËØÝÔÖ××ÙÖØ¿±×ѹ×ÔÒÐÓØÓÒºDynamic deformation at the wing tip (metres)0.00810 Hz Comp.0.007Experiment15 Hz Comp.0.05Original model20 Hz Comp.Stiffened model25 Hz Comp.0.00610 Hz Expt.0.0415 Hz Expt.20 Hz Expt.0.00525 Hz Expt.0.030.004´µÓÑÔÖ×ÓÒÓÝÒÑØÔÓÖ¹0.003ÑØÓÒÛØ«ÖÒØÅÑÓÐ׺0.020.0020.010.001ÙÖº¾½ÓÑÔÖ×ÓÒÓÙÒ×ØÝÔÖ××ÙÖÒÓÖÑØÓÒÖ×ÙÐØ×ØÛÒØÓÖÒÐÒ ´µÍÒ×ØÝÔÖ××ÙÖر×ѹ010 15 20 250 0.25 0.5 0.75 1ØÒÛ×Ø«Ò×ØÖÙØÙÖÐÑÓÐ×ÓØËË̺ ×ÔÒÐÓØÓÒºFlap Oscillating FrequencyLocal chord at 74% semi-spanMagnitude of unsteady pressure (non dimensionalised)