Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
ÐÒØÓÑÓ¬ØÖÑ× ÜÜ ÝÝ ´·Ìµ¾Ù ´·Ìµ¾Ú Ü Ý ÜÝ ÞÞ ´·Ìµ¾Û Ý·Ú Þ ¾¿Ù Ü·Ú Ý·Û Þ·¾¿ÜÞ ÝÞ ´·ÌµÚ ´·ÌµÙ Þ·ÛÝ ÜÕÜ ´¾º½¼µÕÝ ÜÕÞ ´ ½µÅ¾½½ÈÖ·Ì ÈÖÌÌ Ý¾º¾º¿ÙÖÚÐÒÖÓÖÑ Þ ´¾º½½µÓÓÖÒØ×Ý×ØÑ×ÒØÖÓÙ× ÓÖÒØØÓÒÒÒ×ØݺØÖÒ×ÓÖÑØÓÒÖÓÑØÖØ×ÒÓ¹ÓÖÒØ×Ý×ØÑØÓØÐÓÐ ÌÑÓÐÕÙØÓÒ×ÖÛÖØØÒÒÙÖÚÐÒÖÓÖÑØÓÐØØÙ×ÓÒÖ×ÓÖØÖÖÝÐÓдÜÝÞµ ´ÜÝÞµ ´ÜÝÞµÌÂÓÒØÖÑÒÒØÓØØÖÒ×ÓÖÑØÓÒ×ÚÒÝ ØØÌÕÙØÓÒ¾º½ÒØÒÛÖØØÒ× Â´µÏØ·´ Úµ ´ÜÝÞµ ·´ Úµ ·´À ÀÚµ¼ ´¾º½¾µ½¿
Ûֽ ÏÏ ½Â Ü·Ý·ÞÀ¡À½Â Ü·Ý·ÞÀ¡Ú½Â´ÜÚ·ÝÚ·ÞÀÚµ Ü·Ý·ÞÀ¡ ´¾º½¿µÀڽ´ÜÚ·ÝÚ·ÞÀÚµ ڽ´ÜÚ·ÝÚ·ÞÀÚµÌÜÔÖ××ÓÒ×ÓÖØÒÚ×ÙÜ×Ò×ÑÔЬݬÒÒ ÎÜÙ·ÝÚ·ÞÛ ÍÜÙ·ÝÚ·ÞÛÌÒÚ×ÙÜ×ÒØÒÛÖØØÒ× ÏÜÙ·ÝÚ·ÞÛ ´¾º½µ ¼ ÙÍ·ÜÔ ÚÍ·ÝÔ Í ½ ÛÍ·ÞÔ ÍÀ ¼ ÙηÜÔ ÚηÝÔ Î ½ ÛηÞÔ ÎÀ ´¾º½µÀ ¼ ÙÏ·ÜÔ ÚÏ·ÝÔ Ï ½ ÌÖÚØÚØÖÑ×ÓÙÒÒØÚ×ÓÙ×ÙÜ×ÖÚÐÙØÙ×ÒØÒÖÙиÓÖÜÑÔÐ ÛÏ·ÞÔÜÜÙ Ù ·ÜÙ ÏÀ¾º¾ºËØÝËØØËÓÐÚÖ ·ÜÙ Ì×ÔØÐ×ÖØ×ØÓÒÓÕÙØÓÒ¾º½¾Ð×ØÓ×ØÓÓÖÒÖÝ«ÖÒØÐÕÙØÓÒ×Ò ØѸ ½
- 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: ÒÐÐݸØÐÑÒÖÚ×Ó×ØÝ×
- 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 and 38: ¿º¿ ×Ù×ØÓØÖÒ×ÖÓÖ׺
- Page 39 and 40: Fluid Grid Node−1,1η1,1(x,y)(ξ,
- 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
ÐÒØÓÑÓ¬ØÖÑ× ÜÜ ÝÝ ´·Ìµ¾Ù ´·Ìµ¾Ú Ü Ý ÜÝ ÞÞ ´·Ìµ¾Û Ý·Ú Þ ¾¿Ù Ü·Ú Ý·Û Þ·¾¿ÜÞ ÝÞ ´·ÌµÚ ´·ÌµÙ Þ·ÛÝ ÜÕÜ ´¾º½¼µÕÝ ÜÕÞ ´ ½µÅ¾½½ÈÖ·Ì ÈÖÌÌ Ý¾º¾º¿ÙÖÚÐÒÖÓÖÑ Þ ´¾º½½µÓÓÖÒØ×Ý×ØÑ×ÒØÖÓÙ× ÓÖÒØØÓÒÒÒ×ØݺØÖÒ×ÓÖÑØÓÒÖÓÑØÖØ×ÒÓ¹ÓÖÒØ×Ý×ØÑØÓØÐÓÐ ÌÑÓÐÕÙØÓÒ×ÖÛÖØØÒÒÙÖÚÐÒÖÓÖÑØÓÐØØÙ×ÓÒÖ×ÓÖØÖÖÝÐÓдÜÝÞµ ´ÜÝÞµ ´ÜÝÞµÌÂÓÒØÖÑÒÒØÓØØÖÒ×ÓÖÑØÓÒ×ÚÒÝ ØØÌÕÙØÓÒ¾º½ÒØÒÛÖØØÒ× Â´µÏØ·´ Úµ ´ÜÝÞµ ·´ Úµ ·´À ÀÚµ¼ ´¾º½¾µ½¿