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

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Page 51 and 52: Control surface treatmentsBlended e
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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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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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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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B-F-R Case, Euler Simulation, Mach
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Generalised coordinate (rudder mode
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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