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

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Page 25 and 26: AB×ÖÓÙØÓÙØÒ×ØÔ½ºÒÐ
Page 27 and 28: Ì×ÖÐÙÐØ× ÛÖ×½´µ×¾´
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Page 37 and 38: ¿º¿ ×Ù×ØÓØÖÒ×ÖÓÖ×º
Page 39 and 40: Fluid Grid Node−1,1η1,1(x,y)(ξ,
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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
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¿ººÔÐÓ× ÒÓØÖÓÔØÓÒÓ
Page 55 and 56:
Flap´µFlapWingBlended width of th
Page 57 and 58:
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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º¾º¾ÌÆÄËËÌÖÖÓÛÏÒ Ù
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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
Page 81 and 82:
Magnitude of unsteady pressure (non
Page 83 and 84:
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 =
Page 93 and 94:
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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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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