Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
ÛÖÅ×Ø×ÔÙÒØÓÒÓØÐÑÒØØÔÓÒØÙ×ØÓÒØÖÔÓÐØØ×ÔÐÑÒØ× ÛØÒÒÐÑÒØÒØÖÑ×ÓØÒÓÐÖ×ÓÖÓÑÒºÌÚØÓÖÒÒÖÐØØÓ ØÐÓÐ×ÔÐÑÒØÚØÓÖÕÝØÓÒÒØÚØÝÑØÖܸÒØØÐÑÒØÒÍ×ÒØÖÐØÓÒÒÕÙØÓÒ¿º¸Ø×ÔÐÑÒØÚØÓÖÓÖ×ØÖÙØÙÖÐÓÒ×ØÖÒØÔÓÒØ×Ò ×ØØ×ÛÖØØÒØÖ××ÑÐÝ¸× ÒÕ ´¿ºµÛÖ Õש×Õ ´¿ºµ© ¾ ž¾Å ½½ËÑÐÖÐÝØ×ÔÐÑÒØÚØÓÖÕØØÖÓÝÒÑÔÓÒØ×ÒØÖÑ×ÓØÐÓÐ×Ôй ÅÒÒ º ¿ ´¿ºµÑÒØÚØÓÖÕÒÛÖØØÒ×ØÎËØÓÔ××ØÖÓÙÚÒ×ØÓ×ÔÐÑÒØ×Õ×ØÔÒÐØÝÑØÓÓÓÒ×ØÖÒØ×´× ÛÖ©×Ø×ÔÐÑÒØÑÔÔÒÑØÖÜÖÓÑØÎËØÓØÙ×ÙÖÖºÌÓÓÖ Õ©Õ ´¿ºµ×ÖÒ¾℄µÚ×ØÕÙÐÖÙÑ×ØØÓØ×ØÖÙØÙÖºØ×ØÖÙØÙÖÐÖ¸ÒÆ×ÔÒÐØÝÔÖÑØÖºËÓÐÚÒÓÖÕÒ×Ù×ØØÙØÒÒÕÙØÓÒ ÛÖÃ×Ø×Ø«Ò××ÑØÖÜÓØÎ˸©××Ø×ÔÐÑÒØÑÔÔÒÑØÖÜÓØÎËØÓ Ã·Æ©Øש×℄ÕÆ©Ø×Õ× ´¿ºµ¿º¸Ø×ÔÐÑÒØ×ØØÙ×ÙÖÖÔÓÒØ×ÒÜÔÖ×××ÛÖ ÕÌÕ× ´¿º½¼µ¿º¿º¿ÁÒÚÖ×Á×ÓÔÖÑØÖÅÔÔÒ Ì©´Æ ½Ã·©×̩׵ ½©×Ì ´¿º½½µÌ×ÓÔÖÑØÖÑÔÔÒØÒÕÙ×ÛÐÝÙ×ÒÅÒÐÝ××ØÓØÖÒ×ÓÖÑ×ØØÚÖÐ× ÁÒØ×ÔÔÖÓØ×Ñ×ÔÙÒØÓҴƵ×Ù×ØÓÒØÖÔÓÐØØÖÓÝÒÑÖ ÔÓÒØÒØÓÔÔÖÓÜÑØØ×ØÖÙØÙÖÐÓÖÑØÓÒºÌ×ÓÔÖÑØÖÑÔÔÒ×ÖÓÑ Ð×ÔÐÑÒظ×ØÖ××ÒÐÓ×ÖÓÑ×ØÖÙØÙÖÐÖÔÓÒØ×ØÓØÖÓÝÒÑÖÔÓÒØ׺ÐÓÐÓÓÖÒØ´µØÓÐÓÐÓÓÖÒØ×Ý×ØÑ´ÜݵºÌÑÔÔÒÓÒÖÓÝÒÑ ÒÖÓÝÒÑÔÓÒØÐÝÒÒÕÙÖÐØÖÐ×ØÖÙØÙÖÐÐÑÒØ´ÙÖ¿º¿º¿µºÌÐÓÐ ÓÓÖÒØ×ÓÖ×ÙÔÓÒØÒ¬Ò× ÔÓÒØ׬ÒÝØ×ÔÙÒØÓÒ×ÓÖ×ØÖÙØÙÖÐÐÑÒØÛØÒÛØÐ׺ÓÒ×ÖÜÆ´µÜ½ ¿½ ´¿º½¾µ
Fluid Grid Node−1,1η1,1(x,y)(ξ,η)ξÙÖ¿ºÁ×ÓÔÖÑØÖÌÖÒ×ÓÖÑØÓÒ−1,−11,−1ÝÆ´µÝ½ ´¿º½¿µStructural Elementƾ´µ½´½·µ´½ Æ¿´µ½´½·µ´½·µ Æ´µ½´½ µ´½·µ´ÑѵÓØÖÓÝÒÑÔÓÒØ×ÓÒØÓÖÑ×ØÖÙØÙÖÐÖÖÐÙÐØ×ÓÐÐÓÛ׺ ØÖÐÙÐØÒØÐÓÐØÖÒ×ÓÖÑÖÓÝÒÑÓÓÖÒØ×ØÐÓÐÓÓÖÒØ× ´¿º½µÒÖØÖÖÝÐÒÈÉ׬Ò×ÙØØØÐ×ÓÒØÖÓÝÒÑÔÓÒØÅÒÓÒÒÐÑÒØ ÒÓȺÌÐÒØÖÒ×ÓÖÑ×ÒØÓȳɳØÖÓÙÒÚÖ×ÑÔÔÒºÌÕÙØÓÒÓÖØÐÒȳɳÛÖØÓÆÒØ×ÖÓÒ×ØÒØ×ÐÙÐØÖÓÑØ×ÔÙÒØÓÒ×ÒØÓÓÖÒØ×¹ ÓÖÒØ×ÓØÐÑÒØÐÒÓ׿℄ºÇÒØÐÓÐÓÓÖÒØ×¹ÓÖÒØ×ÓÖØØÖÒ×ÓÖÑ ÖÓÝÒÑÖÔÓÒØ´ÑѵÖÐÙÐØØÒØØÖÒ×ÓÖÑÔÐÒÖ×ÔÐÑÒØ×´ÙÚµ ÖÓØÒÝ×ÓÔÖÑØÖÑÔÔÒÚҽƴµÚ½ ÙҽƴµÙ½ ´¿º½µ¿¾ ´¿º½µÛÖ Æ½´µ½´½ µ´½ µÒÛÖØØÒ× ¾··¼ ´¿º½µ
- Page 1 and 2: ÖÓÐ×ØÒÐÝ××ÓÖÖØ ÛØÓ
- Page 3 and 4: ×ØÖØÒØ×Ò×غÍÒØÐØÚ
- Page 5 and 6: ÓÒØÒØ×½ÁÒØÖÓÙØÓÒ ½
- Page 7 and 8: º¿ÄÑØØÓÒÓÄÒÖÖÓÝÒÑ
- Page 9 and 10: ÔÔÐÖÓÝÒÑÓÖ׺ÌÖÓÝÒ
- Page 11 and 12: ÒÚÓÐÚØÖÒ×ÓÒÓÒØÖÓÐ
- Page 13 and 14: ÌÑÓØÚØÓÒÓÖØÙÖÖÒØÛ
- Page 15 and 16: ÓØÒ×ØÐØÝÓÙÒÖÝØØÖÒ
- Page 17 and 18: ¾º¾º½ÆÓÒ¹ÑÒ×ÓÒÐÓÖ
- Page 19 and 20: ÒÐÐݸØÐÑÒÖÚ×Ó×ØÝ×
- Page 21 and 22: Ûֽ ÏÏ ½Â Ü·Ý·ÞÀ¡
- Page 23 and 24: ÇÒØÓØÖÒ¸ØÖØÚØÒÕÙ×
- Page 25 and 26: AB×ÖÓÙØÓÙØÒ×ØÔ½ºÒÐ
- Page 27 and 28: Ì×ÖÐÙÐØ× ÛÖ×½´µ×¾´
- Page 29 and 30: ÒÖÐÙÐØÖÓÑ ÌÙÒØÓÒ×Ò
- Page 31 and 32: Å××ÒÖÐ×ØÓÒ×ÔÖÓÖÑØ
- Page 33 and 34: ÌÖÒ×ÓÖÑØÓÒÅØÓÓÐÓÝ
- Page 35 and 36: ÙÖ¿º¾ÖÐÓÔÓÒØ×ÖÐÝÖ
- Page 37: ¿º¿ ×Ù×ØÓØÖÒ×ÖÓÖ׺
- Page 41 and 42: ÕÙØÓÒ¿º¾ÒÙ×ÓÒÐÝØÒ
- Page 43 and 44: ÁØÛ×ÓÙÒÒ℄ØØØÐÒÖ×Ø
- Page 45 and 46: BBPÙÖ¿ºËÖ××ÛÒÔÐÒÔÖÓ
- Page 47 and 48: X1s,kPurely translated fictitious p
- Page 49 and 50: Structural ComponentLevel 1 Mapping
- Page 51 and 52: Control surface treatmentsBlended e
- Page 53 and 54: ¿ººÔÐÓ× ÒÓØÖÓÔØÓÒÓ
- 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
- Page 63 and 64: ÎÐØÓÒÓÖÓÖÐÔÅÓØÓÒ×
- Page 65 and 66: ÙÖº½ÌÌÛÒØÙÒÒÐÑÓÐÛ
- Page 67 and 68: º¾º¾ÌÆÄËËÌÖÖÓÛÏÒ Ù
- Page 69 and 70: WingDeflected flapØØØÖÙÖÕÙ
- Page 71 and 72: ÐÒ¸ØÛÒØÔÒÐ×ÓÖÓÙÒØ
- Page 73 and 74: ÑÓÖ×¾ØØÖ×ÓÒÒØÖÕÙÒ
- Page 75 and 76: ´µËØÖÙØÙÖÐÑÓÐY:´µÅ
- 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
- Page 87 and 88: ÓÒØÖÓÐËÙÖÁÒ×ØÐØÝ Ô
Fluid Grid Node−1,1η1,1(x,y)(ξ,η)ξÙÖ¿ºÁ×ÓÔÖÑØÖÌÖÒ×ÓÖÑØÓÒ−1,−11,−1ÝÆ´µÝ½ ´¿º½¿µStructural Elementƾ´µ½´½·µ´½ Æ¿´µ½´½·µ´½·µ Æ´µ½´½ µ´½·µ´ÑѵÓØÖÓÝÒÑÔÓÒØ×ÓÒØÓÖÑ×ØÖÙØÙÖÐÖÖÐÙÐØ×ÓÐÐÓÛ׺ ØÖÐÙÐØÒØÐÓÐØÖÒ×ÓÖÑÖÓÝÒÑÓÓÖÒØ×ØÐÓÐÓÓÖÒØ× ´¿º½µÒÖØÖÖÝÐÒÈÉ׬Ò×ÙØØØÐ×ÓÒØÖÓÝÒÑÔÓÒØÅÒÓÒÒÐÑÒØ ÒÓȺÌÐÒØÖÒ×ÓÖÑ×ÒØÓȳɳØÖÓÙÒÚÖ×ÑÔÔÒºÌÕÙØÓÒÓÖØÐÒȳɳÛÖØÓÆÒØ×ÖÓÒ×ØÒØ×ÐÙÐØÖÓÑØ×ÔÙÒØÓÒ×ÒØÓÓÖÒØ×¹ ÓÖÒØ×ÓØÐÑÒØÐÒÓ׿℄ºÇÒØÐÓÐÓÓÖÒØ×¹ÓÖÒØ×ÓÖØØÖÒ×ÓÖÑ ÖÓÝÒÑÖÔÓÒØ´ÑѵÖÐÙÐØØÒØØÖÒ×ÓÖÑÔÐÒÖ×ÔÐÑÒØ×´ÙÚµ ÖÓØÒÝ×ÓÔÖÑØÖÑÔÔÒÚҽƴµÚ½ ÙҽƴµÙ½ ´¿º½µ¿¾ ´¿º½µÛÖ Æ½´µ½´½ µ´½ µÒÛÖØØÒ× ¾··¼ ´¿º½µ