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

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Page 3 and 4: ×ØÖØÒØ×Ò×ØºÍÒØÐØÚ
Page 5 and 6: ÓÒØÒØ×½ÁÒØÖÓÙØÓÒ ½
Page 7 and 8: º¿ÄÑØØÓÒÓÄÒÖÖÓÝÒÑ
Page 9 and 10: ÔÔÐÖÓÝÒÑÓÖ×ºÌÖÓÝÒ
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: ÒÐÐÝ¸ØÐÑÒÖÚ×Ó×ØÝ×
Page 21 and 22: ÛÖ½Â ÏÏÂ 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: ÙÖ¿º¾ÖÐÓÔÓÒØ×ÖÐÝÖ
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
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
Page 105 and 106:
Unsteady force on the flap (nondime
Page 107 and 108:
20152010Flap angle [degrees]50-5-10
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ÌÖ×ØÖÑÚÐÓØÝ×½¾Ñ»×
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×ØÖÙÖÕÙÒÝÚÒÝ¾ ÛÖØ×
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ÌÀÛÖÖØ½ ÔØÖº½ ÁØ×Ò
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ÐÙÐØÓÒ¸ØØÑ×ÛÖ×ÓÒ×
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ÙÖº¿Ù×ÐÜÙÖÐÜ×ÛØØ
Page 119 and 120:
ÖÕÙÒÝÀÞ℄ ½¾º¾ ½º¾
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× ÓÑØÔ ÏÒÛØÔ¼Æ ½¾
Page 123 and 124:
×ÐÐÓÛº ÚØÝ×ÓØÔÐÒ×
Page 125 and 126:
ÅÓ½½¾º ÅÓ¾¿º ÖÕÙÒÝ
Page 127 and 128:
CFDNastranDynamic pressureBuzz regi
Page 129 and 130:
ÙÖº½ØØÓÛÐÐÐÓÒØÔ
Page 131 and 132:
ÖÖØ¸ÒÒØ×ÖÙ×ÓÖØÐÙÐ
Page 133 and 134:
The Hawk Body-Fin-Wing-Rudder CaseO
Page 135 and 136:
ÅÖÖÓÖÒÓÅÓ× ÌØÖØÑÒØ
Page 137 and 138:
×½½½Æ ×¾ ÁÒÒÅÒÙÑÖ ¼
Page 139 and 140:
ÓÖØÖ××ÓÒÖ×ÒÓÑØÖÓÑ
Page 141 and 142:
Spanwise locations on the fin of th
Page 143 and 144:
-Cp on the fin at Y=2.4 MetresBAE-F
Page 145 and 146:
B-F-R Case, Euler Simulation, Mach
Page 147 and 148:
CFDLinearB-F-R (Onset of buzz)B-F-R
Page 149 and 150:
Generalised coordinate (rudder mode
Page 151 and 152:
ÛÖÒÓØÔÖØÝØÙÐÖÕÙØÓ
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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