Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
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Magnitude <strong>of</strong> unsteady pressure (non dimensionalised)0.050.040.0310 Hz Comp.15 Hz Comp.20 Hz Comp.25 Hz Comp.10 Hz Expt.15 Hz Expt.20 Hz Expt.25 Hz Expt.0.02´µÍÒ×ØÝÔÖ××ÙÖØ¿±×ѹ×ÔÒÐÓ¹ ØÓÒº0.010 0.25 0.5 0.75 1Local chord at 38% semi-spanMagnitude <strong>of</strong> unsteady pressure (non dimensionalised)0.050.040.0310 Hz Comp.15 Hz Comp.20 Hz Comp.25 Hz Comp.10 Hz Expt.15 Hz Expt.20 Hz Expt.25 Hz Expt.0.02´µÍÒ×ØÝÔÖ××ÙÖر×ѹ×ÔÒÐÓ¹ ØÓÒº0.010 0.25 0.5 0.75 1Local chord at 74% semi-spanMagnitude <strong>of</strong> dynamic deformation [meters]0.0150.0140.0130.0120.0110.010.0090.00810 Hz Comp.15 Hz Comp.20 Hz Comp.25 Hz Comp.10 Hz Expt.15 Hz Expt.20 Hz Expt.25 Hz Expt.0.00700.0060.005-50´µÍÒ×ØÝÓÖÑØÓÒÐÓÒØ×ÔÒ´×0.0040.003ÙÖº½µº0.002-1000.0010-150ÙÖº¾ÍÒ×ØÝÔÖ××ÙÖÒÓÖÑØÓÒÔÐÓØ×ÓÖØËËÌ×½ÓÑÔÙØØÓÒ×Ù×Ò ´µÈÖ××ÙÖÔ×ÐØÓ½ÀÞº-0.0010 20 40 60 80 1000 0.25 0.5 0.75 1Percentage semi-spanLocal chords at 38% and 74% semi-spansØÊÆËÕÙØÓÒ׺Phase angle [degrees]1501005038% sem-span Comp.74% semi-span Comp.38% semi-span Expt.74% semi-span Expt.
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