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

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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.
Page 61 and 62: Rigid fuselageHierarchy level 1Wing
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Page 69 and 70: WingDeflected flapØØØÖÙÖÕÙ
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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
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Page 91 and 92: 3020∆ t = 0.1∆ t = 0.05∆ t =
Page 93 and 94: 15Flap with gapsBlended flap30Flap
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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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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
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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