Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
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12.07.2015
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Flap´µFlapWingBlended width of the flapWingBlended width of the flapÙÖ¿º½ÌÖÒ×ÓÖÑÔÑÓÙ×ÒØÛÓ«ÖÒØÚÐÙ×ÓÐÒÒÔÖÑØÖ ´µBlending parameter used = -20Blending parameter used = -100ÙÖ¿º½ÈÓ×ØÓÒÓØ×ÐÓÒجҹÖÙÖ
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- Page 5 and 6: ÓÒØÒØ×½ÁÒØÖÓÙØÓÒ ½
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- 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 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: ¿ººÔÐÓ× ÒÓØÖÓÔØÓÒÓ
- 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
- Page 89 and 90: ÅÓ ÏÒÒÒ ÐÔÇ×ÐÐØÓÒ ½
- Page 91 and 92: 3020∆ t = 0.1∆ t = 0.05∆ t =
- Page 93 and 94: 15Flap with gapsBlended flap30Flap
- Page 95 and 96: 0.020.020.0150.015Generalised Coord
- Page 97 and 98: 0.020.02Generalised Coordinate0.010
- Page 99 and 100: 10.90.00250.8Generalised Coordinate
- Page 101 and 102: 4040Initial grid velocity 0.02Initi
- Page 103 and 104: Unsteady force on the flap0.00100.0
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