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- W2259938053 abstract "For the flutter analysis it is demanding that the deformation of mode shapes istransferred to the aerodynamic grid to analyse unsteady aerodynamic loads inducedby the oscillation. If the analysis is based on measurements, the available informationof deflections is limited to the applied transducers which will generally measure theacceleration in one translation direction. In general about 100 sensors are applied forsmall two and four seated aircrafts and gliders and about 200 are used for aircrafts inthe CS23 category.For the interpolation of the measured acceleration amplitudes it was assumed thateach wing section is rigid in the flow direction. For span-wise interpolation one dimensional cubic splines are applied for each aircraft component to analyze thevarying bending, in-plane bending and torsion from root to tip. As the sensors canonly measure translational accelerations the twist of the lifting surfaces must becalculated from amplitude differences at leading edge, trailing edge and hinge line,respectively. In addition the deflection angles of control faces with respect to the wingare calculated." @default.
- W2259938053 created "2016-06-24" @default.
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- W2259938053 date "2010-02-02" @default.
- W2259938053 modified "2023-09-23" @default.
- W2259938053 title "Interpolation of GVT Results using Volume-Spline Method" @default.
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- W2259938053 hasPublicationYear "2010" @default.
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