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

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Flap´µFlapWingBlended width <strong>of</strong> the flapWingBlended width <strong>of</strong> the flapÙÖ¿º½ÌÖÒ×ÓÖÑÔÑÓÙ×ÒØÛÓ«ÖÒØÚÐÙ×ÓÐÒÒÔÖÑØÖ ´µBlending parameter used = -20Blending parameter used = -100ÙÖ¿º½ÈÓ×ØÓÒÓØ×ÐÓÒØ¬Ò¹ÖÙÖ
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Page 35 and 36: ÙÖ¿º¾ÖÐÓÔÓÒØ×ÖÐÝÖ
Page 37 and 38: ¿º¿ ×Ù×ØÓØÖÒ×ÖÓÖ×º
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
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Page 65 and 66: ÙÖº½ÌÌÛÒØÙÒÒÐÑÓÐÛ
Page 67 and 68: º¾º¾ÌÆÄËËÌÖÖÓÛÏÒ Ù
Page 69 and 70: WingDeflected flapØØØÖÙÖÕÙ
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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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Unsteady force on the flap (nondime
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20152010Flap angle [degrees]50-5-10
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CFDNastranDynamic pressureBuzz regi
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The Hawk Body-Fin-Wing-Rudder CaseO
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×½½½Æ ×¾ ÁÒÒÅÒÙÑÖ ¼
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Spanwise locations on the fin of th
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-Cp on the fin at Y=2.4 MetresBAE-F
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B-F-R Case, Euler Simulation, Mach
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CFDLinearB-F-R (Onset of buzz)B-F-R
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Generalised coordinate (rudder mode
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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