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

×ÙÔÖ×ÓÒÅÒÙÑÖ×Ò×ÙØ×ÓÒÙÙÞÞÒ×ØÐØݺÙÖº¿×ÓÛ×Ø ÚÖØÓÒÓØ×Ó×ØÖÒØØ×ÔÒÐÓØÓÒÓݾº¾ºÑØÖ׺ÁØÒ×ÒØØØÒØÒÐÝ××Ø­ÓÛÐÖØ×ÓÚÖØÛÒ×ÒÛÒجÒÐÐÝÖ×جÒØ ×ÓÒÖ××Ò×ØÖÒØÒØÐÐÝÒÙØÛÒ××ØÅÒÙÑÖÒÖ×׺×ØÖÚÐÓØÝØÒØÖ×ØÖÑÚÐÓØݺØÙÔÔÖ×ÙÔÖ×ÓÒÅÒÙÑÖ×Ø ÁÒØ×Ù×ÓÒÖÓÒÔÖØ×ÐÓÛÖ­ÙØØÖÚÐÓØÝØÒÐÒÖºÌ××Ù×ÒØÖÖÒ«ØÓØÛÒÓÒجÒ×ÑØÓÖÙÒÓÓÓÑÔÖ×ÓÒØÛÒÐÒÖ Ò×­ÙØØÖÚÐÓØÝ×ÓØÒº ÓÒع¹Ê¸¹¹Ê¹ÌÒ¹¹Ï¹Ê¹Ì×׺××ÒÒØ×ØÝ­ÓÛ×ÑÙÐØÓÒ×Ø ÒØÖÖÒ«Ø×ÓØÓÑÔÓÒÒØ××ÑÓÖ«ØÓÒØ×Ó×ØÖÒØÓÒجÒÒ Ì«ØÓÓÑÔÓÒÒØÒØÖÖÒÛ×ÒÚ×ØØÝÔÖÓÖÑÒÖÓÐ×ØÒÐÝ××ÒØÔÖ××ÙÖ×ØÖÙØÓÒºÅØÔÓÒØÒÐÝ××Û×ÔÖÓÖÑؽ¼¸¼¼¼ØÒØ Å¼ºÓÒØØÖ××ØÓÒÚ×ØØØÔÖ×ÒÓØÙÞÞÒ×ØÐØݺÙÖº¿ ×ÓÛ×ØÑÓÐÖ×ÔÓÒ×ÓØÖÙÖÖÓØØÓÒÑÓºÁØ××ÒØØÓÖØÓÑÔÐØ߹Ϲ ʹÌ×ØÒØÐÔÖØÙÖØÓÒÑÔ×ÓÛÒÒØѺÁÒÙÖ׺¿¿Òº¿Ø¹¹Ï¹Ê¹Ì ×ÒÓÑÔÖ×ÓÒØÓØÓØÖØÛÓ×××ØÛ×Ø×Ӻ̹¹ÊÒع¹ ʹÌ××ÓÙÒÖÓÙÞÞØżºÙØÓØÔÖ×ÒÓØ×ÓºÁØ××ÒØØ ØÑÔÐØÙÓÓ×ÐÐØÓÒ×ÖØÖÓÖع¹Ê¹Ì××ØÔÖ×ÒÓØÐÒ× Ø×ÓÐÓØÓÒØÓØÖÙÖØÖÐÒ´×ÙÖº¿µºÌÓÖØÐÐÝØÙÞÞÓÒ×Ø ÓÙÖ×ÑÙÖÐÖÓÖع¹ÊÒ¹¹Ê¹Ì××ØÒع¹Ï¹Ê¹Ì×׺ÙÖº¿ ×ÓÛ×ØÝÒÑÒ×ØÐØÝÓÙÒÖÝÓع¹Ï¹Ê¹Ì׺ÁÒØ×Ù×ÓÒÖÓÒØÖ ×­ÙØØÖØÝÔÒ×ØÐØݸººÒÙÒÑÔÒ×ØÐØÝÒÒÓØÒÄǸÔÖØÛ ÓÑÔÖ×Ö×ÓÒÐÝÛØØÐÒÖÑØÓºÙÖº¿×ÓÛ×ØÑÔÒÙÒÑÔ ÑÓÐÖ×ÔÓÒ××ÓÖØÛÓÝÒÑÔÖ××ÙÖ×ØżººÍÒÐØÄÇØÝÔÒ×ØÐØÝØ Ö×ØÓÖØÓÒ׺ÔÒØÝÒÑÔÖ××ÙÖÚÐÓÔ×ÛØÒÖ×ÒÅÒÙÑÖÒØ ÑÔÐØÙÓØ­ÙØØÖÓ×ÐÐØÓÒ×ÔÖÓÛÒÙÒØÐØÐÙÐØÓÒ×ÖÓÛÒÙ×ÚÖ ÖØÒØÖÒ×ÓÒÅÒÙÑÖØÒ×ØÐØÝÓÑ×ÒÄÇØÝÔºÌÐÒÖÒÐÝ×× ×ÙÒÖÐÐÐÓ×ØÓÅÒÙÑÖ½ºÀÓÛÚÖÛÖÐÒÖÖ×ÙÐØ×ÖÔØÐØÖ×ÔÖØÓÒÔÐØÝÓÐÒÖ×ÖÓÝÒÑ׺ÇÒØ×ÓÙ××ØÖÅÒÙÑÖ Ö×ØÖÑÅÒÙÑÖ׺Ì××Ù×ØÒ×ØÐØÝ××ÓÒÙÒ×ÝÓÒØ «ÖÒØÛÒØÓÙÒÖ×ÔÖØÝÒØÐÒÖÑØÓØ×ÙÔÖ×ÓÒØÐÒÖÒÔÖØÓÒ×ÒØÓÑØÙÔºÙÖº¿×ÓÛ×ØÔÖ××ÙÖ×ØÖÙØÓÒ ÓÒع¹Ï¹Ê¹Ì×ؾº¾ÑØÖ××ÔÒ´×ÙÖº¾µØÖÒÓÅÒÙÑÖ׺ÁØÒ ×ÒØØØ×Ó××ÒØÓÒØÖÙÖØÐÓÛØÖÒ×ÓÒÅÒÙÑÖ×ÒØÒ×ØÐØÝ ×ÓØ­ÙØØÖØÝÔºØÙÔÔÖØÖÒ×ÓÒÅÒÙÑÖ×Ø×Ó×ØÖÒØÒ×ÓÒØÖÙÖ Ö×ÙÐØÒÒÙÞÞºØÙÔÔÖ×ÙÔÖ×ÓÒÅÒÙÑÖ×Ø×Ó«Ù××ÓÚÖجҹÖÙÖÒ ÙÞÞ×ÔÔÖ׺ º ÌÒÐÝ××ÒØÙÖÖÒØÔØÖ×ÔÖÓÚÙ×ÙÐÒ×Ø×ÒØÓØÑÓÐÐÒÓÖÓÐ×Ø ××ÓÖØÔÖØÓÒÓÙÞÞØÝÔÒ×ØÐØ׺ ÓÒÐÙ×ÓÒ×ÁØÛ××ÒÒØÒÚ×ØØÓÒÓØÓÑØ­ÔÓÒ¬ÙÖØÓÒØØØØÖÒ×ÓÒÒÙÑÖ× ½¿¿