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

×ØÖÙÖÕÙÒÝÚÒݾ ÛÖØ×ØÖÒ×ØݸÍ×ØÖ×ØÖÑÚÐÓØݸ¬×Ôž ÔÓØÒØЫÖÒÓÚÒÐÓÛØÖÓÝÒÑÔÒÐÒ×ÚÒݨ¨ÓÚ ½¸¨×ØÑÓ¬ÖÙÖÕÙÒÝÒ׬Ò׼ŬҬÒÐÐÝÅ×ØÅÒÙÑÖºÁÒÕÙØÓÒº¾ Í ÛÖ×ØÖÕÙÒÝÓØÑÓ¸¼×ØÑÓ¬ ¾¨ÐÓÛØÒ×ÒØØ×ØÅÒÙÑÖÔÔÖÓ×½ØØÖѽ¬ÔÔÖÓ×Ò¬ÒØÝÖÒÖÒ ÖÕÙÒÝÒ×ÒØÒÙÑÖÓÔÒÐ×Ù×ØÓÖ×ÓÐÚØ­ÓÛ×ÔÖÓÔÓÖØÓÒÐØÓØÖÙ ØÐØÐÙÐØÓÒÒÚкÈÝ×ÐÐÝØ×Ø«ØÓÒÖ×ÒØÚÐÙÓØÖÙ ÖÕÙÒÝØÓÖØÐÐÝÚÖÝÐÖÒÙÑÖÓÔÒÐ×ÖÖÕÙÖÓÖ­ÓÛÒÐÝ××ØÅ ÒÙÑÖ×ÔÔÖÓÒ½ØÓØÑÒÒÙÐÖ×ÙÐØ׺ÙÖØÖÚÐÓÔÑÒØ×ÓÇƽÚÒÚÐÓÔÑÒØ×ÖÒÓØÒÓÖÔÓÖØÒØÓÖÒÐÇƽÑØÓÓÐÓÝÙ×ÒÆËÌÊÆÛ ×ÙÔÖ×ÓÒÅÒÙÑÖ×℄Ò×ÑÔÐÑÒØÒØÊÇÔ¿℄ºÀÓÛÚÖØ× ÑÛØÖÓÖÑÙÐØÓÒÓÐÙÐØÓÒÓØÙÒ×ØÝÐØØØ××ÓÐÚØ×ÐÑØØÓÒØÐÓÛ×ØÐÒÖØÓÓÐÙ×ÒØÙÖÖÒØÛÓÖºÁØ×ÓÙÐÐ×ÓÒÓØØØØØØÒÐÙ×ÓÒÓØ ÓÒØÖÓÐ×ÙÖÖÓØØÓÒÑÓ×Ø×ÓÙÖÓÒ×ØÐØÝØØÐÓÛ×ÙÔÖ×ÓÒÅÒÙÑÖ× ÒØØ×ÑØÙØÓØÒØÚÑÔÒÓ×ÖÚÒ×ÙÔÖ×ÓÒÐÒÖÒÐÝ××ÓÖ ÔÒÓÑÒÓÒÒÆËÌÊÆÖÕÙÖ×ØÐ×ÓÇƽÛ×ÙÒÚÐÐÒÐØÖØÙÖº ÖÓÓÐ×ÙÒÖÓÒÔØÓ×ÐÐØÓÒ×ÓÙØØ×ÐÒ¿℄ºÒÜØÜÔÐÒØÓÒÓØ׺ ÑØÓÓÖ×ÑÙÐØÓÒÓ¿ÙÞÞÛ×ÑÓÒ×ØÖغÔÖØÖÓÑØÔÖØÓÒÓØ Ò×ØÐØÝÓÙÒÖݸÙÞÞÔÖÑØÖ×ÐÑÔÐØÙ¸ÖÕÙÒÝÒ«ØÓÑÔÒÛÖÐ×Ó ÓÒÐÙ×ÓÒ×Ñ×ÙÖÙ×ÒØÙÐÖÒÊÆËÕÙØÓÒ׺ÙÞÞ×ÑÙÐØÓÒ×Ù×ÒØÙÐÖÕÙØÓÒ× ÛÖÔÖÓÖÑÓÒÐÒ­Ô×Ò­Ô×ÛØÖ×ÒØ­ÔÖ×ÔÓÒ×Û×ÓÙÒØÓ ×ÑÐÖº×ØÖÓÒÔÒÒÓØÙÞÞÓÒ×ØÓÒØÒØÐÑÔÙÐ×Û×Ó×ÖÚºÖÓÑ ÒÚ××ÑÙÐØÓÒ×ØÛ×ÓÒÐÙØØÐØÓÙØÝÒÔÖØØÓÒ×ØÓÙÞÞ¸ØÝ ÒÒÓØÙÖØÐÝÔÖØØÙÞÞÔÖÑØÖ×ÐÑÔÐØÙÒÖÕÙÒݺÐÓÛ×ÔÖØÓÒ ÓÚÖØÓ×ÐÐØÒ­Ô×ÒÒ­ÙÒÓÒØ×ÔÖÑØÖ×ÒÒÚ×Ó×ØÝ«Ø×ÒØÓ ÑÓÐкÓÒ××ØÒØÛØÜÔÖÑÒØÐÓ×ÖÚØÓÒ×ØÑÔÐØÙÓÄÇÔÖØÝØ ÊÆËÕÙØÓÒ×Û×ÓÙÒØÓ×Ò×ØÚØÓØÊÝÒÓÐ×ÒÙÑÖÒØÖÙÖÕÙÒÝ ÓØ­Ôº Ì«ØÓÓÒØÖÓÐ×ÙÖÓÒØ­ÙØØÖÓØÛÒÛ×ÒÚ×ØØÒØÛ×ÓÙÒØÓÖÙ Ø­ÙØØÖÚÐÓØÝ×Ò¬ÒØÐÝÚÒØ×Ù×ÓÒ­ÓÛ××ÓÑÔÖØÓÛÒÛØÓÙØÓÒØÖÓÐ ×ÙÖºÁÒØÖÒ×ÓÒÒ×ÙÔÖ×ÓÒ­ÓÛ×Ø×ÓÒÙÓ×ÐÐØÓÒ×ÓØ­ÔÓÑÒØ ØÖÓÐ×ØÖ×ÔÓÒ×ÓØÛÒØØÒØÖÕÙÒÝÓÓ×ÐÐØÓÒ׺ÐÓÒÛØØÐÒÖ ­ÙØØÖÖ×ÙÐØ×ÓÒØËËÌÖÓÑØ×ÓÒÐÙØØÐÒÖÑØÓ×ÖÙÒÐØÓÔÖØ­ÙØØÖ ØÛÒÅÒÙÑÖ×½º¼Ò½º½ÓÖ××ÛØØÖÐÒÓÒØÖÓÐ×ÙÖºÌÓÙØ× ×ÓÛÒÖØØ×ØÑÑÖÒÒÐÝ×××ÐØÓÔÖØØÒ×ØÐØ×ÙØÓÑØÓÓÖÙÒ×ØÝÖÓÝÒÑ×ÑÒØÒجÐØÝÓØÑÓÐÐÖÓÝÒÑ×ØØ ÖÓÝÒÑÒÓÒÐÒÖØ×ØÖÑÒ×ÓÑÔÙØØÓÒÐÐÝÜÔÒ×ÚºÊÙÇÖÖÅÓдÊÇŵ×ÑØÑÐÓÛÖØÓÑÔÙØØÓÒÐÖ×ÓÖÓÑÔÖ×ÒØÒØÒÙÑÖÐÑÓÐ℄º ØÒÕÙ×ÐÈÖÓÔÖÇÖØÓÓÒÐÓÑÔÓ×ØÓÒ´Èǵ¸ÎÓÐØÖÖØÓÖÝÒÀÓÔÙÖØÓÒÌ×ÚÒÙ×ØÓØÖÑÒØ­ÙØØÖÓÙÒÖ×ÓÛÒ×ÒÖÓÓÐ×ÒØÖÒ×ÓÒ ½¼