Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Xs,kFictitious structural pointj>ÙÖ¿º½¼Ì½Î̬ØØÓÙ×ÔÓÒØXXs,js,i×ÓÐÙØÓÒÛÓÙÐØÓÖØ×ØÖÙØÙÖÐØÖÒÐÝÒÒ¬ØØÓÙ×ÔÓÒØÐÓ×ØÓÓÒ ÑÐÑÒØØ××ÒÓØÔÓ××Ð×Ø×ØÖÙØÙÖÐÔÓÒØ×ÓÒÓØÓÖÑÔÐÒºÇÒÔÓ××Ð2−D triangular element constructed with the fictitious pointOriginal 1−D structural elementÔÓÒØ×ÐÙÐØ×ÕÙÐØÓØ×ÔÐÑÒØÓØÖÐ×ØÖÙØÙÖÐÔÓÒØÐÓ××ØØÓغºØ ÔÓÒØÓÖÑ×ØÖÒÙÐÖÐÑÒغÏÒØ×ØÖÙØÙÖÓÖÑ×Ø×ÔÐÑÒØÓØ׬ØØÓÙ× ÓØ×ØÖÙØÙÖÐÒÓ××ÓØØØØÛÓÒÓ×ÓØÑÐÑÒØÐÓÒÛØجØØÓÙ×ÙÒÖÓ×ÓÒÐÝØÖÒ×ÐØÓÒÛØÓÙØÙ×ØÒØÖÐØÚÔÓ×ØÓÒØÓØÒÒÓØÙ×к ¬ØØÓÙ×ØÖÔÓÒØÓÖØ×ØÖÙØÙÖÐÖÛ×ÒØÖÓÙÓÖ½ÑÐÑÒغÌ× ÔÓÒØØ×ÑÜÒÞÓÓÖÒØ××ÓÒÓØØÛÓÔÓÒØ×ÓÖÑÒؽÐÑÒغÌÝ ÓÓÖÒØÓجØØÓÙ×ÔÓÒØ×ÙÒØÑÓÖØÒØØÓØÓÖÒÐÔÓÒغÙÖ´¿º½¼µ ×ÓÛ×ؽ×ØÖÙØÙÖÐÐÑÒØÓÖÑÝØÔÓÒØ×Ü׸Ü×ÒجØØÓÙ××ØÖÙØÙÖÐØÖÒ×ÐØÓÒØÓØÙÔÓÒØ׺ÆÓÖÓØØÓÒ×ÒØÖÓÙ¸ÓÒ××ØÒØÛØØÑÓØÓÒÓØ ÛÖ×ÙÒØÚØÓÖÒØÖØÓÒÓØݹÜ׺ÌØÖÒÙÐÖÐÑÒØÓÖÑ×ØÒÔÓÒØ×ÓÒØÑ´ÖÖÙÖ´¿º½½µµºÓÒ×ÖØÓÖÑØÓÒÓØÒÓÜ×ÛÒ Ù×ÒØÓÒÚÒØÓÒÐÎÌØÒÕÙ××ÖÒ×ØÓÒ¿ººÌ×ØÒÕÙÚ×ÔÙÖÛÖØ×ÙÔÖ×ÖÔؽҼÖÔÖ×ÒØØÓÖÑÒÙÒÓÖÑ×ØØ×ÓØ×ØÖÙØÙÖÐ ÒÓ׺ÌÓÖѬØØÓÙ×ÒÓÒØÒÐÙÐØ׿º ÙÐÐÖÖØÌÖÒ×ÓÖÑØÓÒ Ü½×ܼ׷ÆÜ× ´¿ºµØÖÒ×ÓÖÑØÓÒÓÖØÓÑÔÐØÖÖØÛØØÑÒÑÙÑÓÑÒÙÐÒØÖÚÒØÓÒÒÛ ÓÖ×ÑÔÐ×ØÒÐÓÒÓÑØÖ×ÐØÛÒºÚÖ×ÓÒÓØÎÌÛÒÓØ ÌÔÖÒ×ØÓÒ×ÚÐØÛØØ×ÓÖÑÙÐØÓÒÓØÎÌÛÒÙ׿ÔÓÒØÜ׺ Ü×Ü×· ´¿ºµÛÖØØÒ× Ü½×ܼ׷ÆÜ× ´¿ºµ
X1s,kPurely translated fictitious point1Xs,j0X Fictitious structural points,kα =/ α 1α 1 1Xs,jα0X X 0s,iDeformed 1−D elementÔÖ×ÖÚ×Ø×ÙÖÑ׸ÔÖØÙÐÖÐÝØÙÒØÓÒ×ØÛÒÓÑÔÓÒÒØ×××ÖÒØs,jÙÖ¿º½½ÌÖÒ×ÐØÓÒÓؽÎÌÐÑÒØÙÖÖÒØ×ØÓÒºÌÒ×ØÓÖØÑØÓ×ÔÖÓÚÝØÔÔÖÓÅÐÚÐÐ℄Û2−D triangular element constructed with the fictitious pointOriginal 1−D structural element××ÓØÛØÓÑÔÓÒÒØ׺ÌÔÖÑÖÝÓÑÔÓÒÒØ×ØÙ×кÌÙÒ×ØÖÙØÙÖÐ ØÖØ×ØÖÖØÓÑÔÓÒÒØ×ÒÖÖݺÖÔÓÒØ×ÓÒØÙ×ÐÖØÖÓÖ×ÒØ×ÒÓÐÚнºÆÜظØÛÒ׸ÓÖÞÓÒØР̬Ö×Ø×ØÓØÑØÓ×ØÓÔÖØØÓÒØÙÒ×ØÖÙØÙÖÐÔÓÒØ×ÒØÓÐÚÐ××ØÐ×ÖÒØÚÖØЬÒÖÓÒÒØØÓØÙ×ÐÒØÙÒ×ØÖÙØÙÖÐÖÔÓÒØ××ÓÒÖÝÑÓØÓÒÙØÓØÖÓÛÒÐ×ØØݺÜØÖÓÑÔÓÒÒØ×ØØØÓØÛÒ¸×Ù ÐÚоÔÓÒØ×ÚÔÖÑÖÝÑÓØÓÒÙØÓØØØØØÝÖÓÒÒØØÓØÙ×ÐÒ ÓÒØ×ÓÑÔÓÒÒØ×ÒØÙ×ÐÖ×ÒØÐÚоºÌÓØÖÖÝ×ØØ×ÔÝÐÓÒ×ÒÓÒØÖÓÐ×ÙÖ×ÛÓÙÐ×ÒØÐÚп¸ÛØØÖÔÖÑÖÝÑÓØÓÒÒÙ ØÓØØØØØÝÖØØØÓØÛÒºÒØ×ØÖÙØÙÖÐÔÓÒØ××ËѺÌÐÓÛ×ØÐÚÐÓÒØÒ×ÐÐÓØÔÓÒØ×ÒØÖ×ÔØÚ Ö׸ÛØÓÒ×Ù×ØÓÖÐÚкÒÓØØ×ØÓÖÓÝÒÑÔÓÒØ×ÒÐÚÐÑ×Ñ ØØ××ØÒÙÑÖÓ×Ù×Ø×ÓÔÓÒØ×ÚÒ¬ÒÓÖØÙÒ×ØÖÙØÙÖÐÖ×ÒÐÚÐÑ ×ØÖÙØÙÖÐÔÓÒØ׺Ì××ÓÒÒÔÖØݬÒÒØÖÒÙÐÖ×ØÓÒÓØ×ØÖÙØÙÖÐÖ Ì¬Ö×Ø×ØÓÖØÎÌ××ÖÓÚ×ØÓ××ÓØÙÔÓÒØÛØØÖ ½××Ù×ØÓÐÚÐѺÒØÒ××ÓØÒØÔÓÒØÛØØÖÒÐ××ÖÒ×ØÓÒ¿ºº½ºÌ×ÑÔÔÒÒÓÒØÙ×кÌÐÚоÑÔÔÒÛÐÐÚØÙ×ÐÒØÐÚоÓÑÔÓÒÒØ×ÐØ ÙÐÐÖÖØ×ØÐÚÐÓÒÑÔÔÒÛÐÐÚÐÐÔÓÒØ×ÒØÙÖÖÚÒÓÒÐÝÝÔÓÒØ× ÓÒÓÚÖØ×ØÖÙØÙÖÐÔÓÒØ×ÒÐÚÐ×ÛÐи¬ÒÒÑÔÔÒ×ÓÖÐÚкÁÒØÖØØØÓºÄÚпÑÔÔÒ×ÕÙÚÐÒØØÓØÓÖÒÐÎÌÑØÓÔÔÐØÓÐÐÖ ÛÒ׸ØÐÒجÒÒÖÚÒÝØÖ×ÔØÚ×ØÖÙØÙÖÐÓÑÔÓÒÒØ×ÛÖ×ØÐÚÐÔÓÒØ×ÛØÓÙØÖ×ØÖØÓÒºÓÒ×ÖÙÐÐÖÖØ×ÚÒØÙ×иØÛÒ׸ØÔ ¿ÓÑÔÓÒÒØ×ÐÔÝÐÓÒ×ÒÓÒØÖÓÐ×ÙÖÛÐÐÑÔÔÝØÐÚоÓÑÔÓÒÒØ×ØÝØØØÓØÛÒ׸ØÔÝÐÓÒØØØÓØÛҸجҸØÖÙÖÒØØÐÔÐÒ ×ÓÑÔÓÒÒØ׺ÙÖ¿º½¾×ÓÛ×Ø×ÑØÓØ¿ÐÚÐ×ÓØÖÒ×ÓÖÑØÓÒØØÐØÓ ¼
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- Page 51 and 52: Control surface treatmentsBlended e
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- Page 55 and 56: Flap´µFlapWingBlended width of th
- Page 57 and 58: WingFlapFlap´µWingGapSheared cell
- Page 59 and 60: Case 3: Mach 0.769, frequency 5 Hz.
- Page 61 and 62: Rigid fuselageHierarchy level 1Wing
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- Page 77 and 78: Case 3: Mach 0.769, frequency 5 Hz.
- Page 79 and 80: Generalised coordinate (wing bendin
- Page 81 and 82: Magnitude of unsteady pressure (non
- Page 83 and 84: P: 0.6 0.666667 0.733333 0.8 0.8666
- Page 85 and 86: Magnitude of unsteady pressure (non
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- Page 93 and 94: 15Flap with gapsBlended flap30Flap
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