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Fluid Grid Node−1,1η1,1(x,y)(ξ,
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ÁØÛ×ÓÙÒÒ℄ØØØÐÒÖ×Ø
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BBPÙÖ¿ºËÖ××ÛÒÔÐÒÔÖÓ
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X1s,kPurely translated fictitious p
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Structural ComponentLevel 1 Mapping
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Control surface treatmentsBlended e
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¿ººÔÐÓ× ÒÓØÖÓÔØÓÒÓ
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Flap´µFlapWingBlended width of th
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WingFlapFlap´µWingGapSheared cell
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Case 3: Mach 0.769, frequency 5 Hz.
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Rigid fuselageHierarchy level 1Wing
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WingDeflected flapØØØÖÙÖÕÙ
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´µËØÖÙØÙÖÐÑÓÐY:´µÅ
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Case 3: Mach 0.769, frequency 5 Hz.
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Generalised coordinate (wing bendin
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Magnitude of unsteady pressure (non
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P: 0.6 0.666667 0.733333 0.8 0.8666
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Magnitude of unsteady pressure (non
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ÓÒØÖÓÐËÙÖÁÒ×ØÐØÝ Ô
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ÅÓ ÏÒÒÒ ÐÔÇ×ÐÐØÓÒ ½
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3020∆ t = 0.1∆ t = 0.05∆ t =
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15Flap with gapsBlended flap30Flap
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0.020.020.0150.015Generalised Coord
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0.020.02Generalised Coordinate0.010
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10.90.00250.8Generalised Coordinate
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4040Initial grid velocity 0.02Initi
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Unsteady force on the flap0.00100.0
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Unsteady force on the flap (nondime
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20152010Flap angle [degrees]50-5-10
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- Page 111 and 112: ×ØÖÙÖÕÙÒÝÚÒݾ ÛÖØ×
- Page 113 and 114: ÌÀÛÖÖؽ ÔØÖº½ ÁØ×Ò
- Page 115 and 116: ÐÙÐØÓÒ¸ØØÑ×ÛÖ×ÓÒ×
- Page 117 and 118: ÙÖº¿Ù×ÐÜÙÖÐÜ×ÛØØ
- Page 119 and 120: ÖÕÙÒÝÀÞ℄ ½¾º¾ ½º¾
- Page 121 and 122: × ÓÑØÔ ÏÒÛØÔ¼Æ ½¾
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- Page 127 and 128: CFDNastranDynamic pressureBuzz regi
- Page 129 and 130: ÙÖº½ØØÓÛÐÐÐÓÒØÔ
- Page 131 and 132: ÖÖظÒÒØ×ÖÙ×ÓÖØÐÙÐ
- Page 133 and 134: The Hawk Body-Fin-Wing-Rudder CaseO
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- 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: ℄ºÃÖÐ××ÓÒÒºÏÒÞÐк