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

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Structural ComponentLevel 1 Mapping
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Control surface treatmentsBlended e
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Flap´µFlapWingBlended width of th
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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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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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