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

Generalised coordinate (wing bending mode)0.050.040.030.020.01timestep 0.14timestep 0.08timestep 0.04Generalised coordinate (wing bending mode)0.0040.0030.0020.001timestep 0.15timestep 0.0600-0.01-0.001´µØÓ½ÀÞÑÔÐØÙÒÖ××ÛØ-0.02Ö×ÒØÑ×ØÔº-0.002-0.03-0.003-0.04ÙÖº½ËÒ×ØÚØÝÓØÑÓÐÖ×ÔÓÒ×ØÓØØÑ×ØÔØØÖ×ÓÒÒÓØËË̸ ´µØÓ¾ÀÞÑÔÐØÙÖÑÒ×ÙÒ¹ ÒÛØÖ×ÒØÑ×ØÔº-0.05-0.0040 50 100 150 200 250 3000 50 100 150 200Nondimensionalised timeNondimensionalised time×½¸ÙÐÖ×ÑÙÐØÓÒº´µÄÓØÓÒÓÙÒ×ØÝÔÖ××ÙÖØÖÒ×ÙÖ׺ ÙÖº½ÄÓØÓÒÓÑ×ÙÖÑÒØÔÓÒØ×ÒØËËÌÜÔÖÑÒØ׺ ÒÑÓÖÑØÓÒº ´µÄÓØÓÒÓÓÔØÐØÖØ×ØÓÑ×ÙÖݹ¾