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- 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: AB×ÖÓÙØÓÙØÒ×ØÔ½ºÒÐ
- 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
- 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
- Page 109 and 110:
ÌÖ×ØÖÑÚÐÓØÝ×½¾Ñ»×
- Page 111 and 112:
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- Page 113 and 114:
ÌÀÛÖÖؽ ÔØÖº½ ÁØ×Ò
- Page 115 and 116:
ÐÙÐØÓÒ¸ØØÑ×ÛÖ×ÓÒ×
- Page 117 and 118:
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- Page 119 and 120:
ÖÕÙÒÝÀÞ℄ ½¾º¾ ½º¾
- Page 121 and 122:
× 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:
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- Page 131 and 132:
ÖÖظÒÒØ×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
- Page 153 and 154:
ÓÒØÖÓÐÐÛÒÓÖÑØÓÒ×Ò
- Page 155 and 156:
½℄ÆËÙÓÑÑØØÓÒÎÖØÓÒ
- Page 157 and 158:
℄úÊÓÙҸźÖÒ̺ÓÖØ
- Page 159 and 160:
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