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

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Unsteady force on the flap0.00400.00200.0000-0.0020-0.0040´µÐÔÙÔÔÖ×ÙÖ-0.0060-0.0080-0.0100-30 -20 -10 0 10 20 30Flap angle [degrees]Normalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force00 5 10 15 20 25 30 35-0.2-0.4´µÐÔÐÓÛÖ×ÙÖ-0.6-0.8Time (nondimensionalised)-1Unsteady force on the flap0.00400.00200.0000-0.002000 5 10 15 20 25 30 35-0.0040-0.2´µÐÔÙÔÔÖ×ÙÖ-0.0060-0.4-0.6-0.0080ÙÖº½¿ÌÙÒ×ØÝÓÖÒÔÑÓØÓÒÛÒÚÒÐÖÒØÐÔÖØÙÖØÓÒºÍÒ×ØÝ-0.8Time (nondimensionalised)ÓÖÚÐÙ×ÖØÒÓÒØÔÙÔÔÖÒÐÓÛÖ×ÙÖ×ºÙÐÖ×ÑÙÐØÓÒØÅ¼ºÒ ´µÐÔÐÓÛÖ×ÙÖ-0.0100-1-30 -20 -10 0 10 20 30Flap angle [degrees]ÝÒÑÔÖ××ÙÖ¾ºÈºNormalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force
Unsteady force on the flap0.00100.00050.0000-0.0005-0.0010´µÐÔÙÔÔÖ×ÙÖ-0.0015-0.0020-4 -3 -2 -1 0 1 2 3 4Flap angle [degrees]Normalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force00 5 10 15 20 25 30 35-0.2-0.4´µÐÔÙÔÔÖ×ÙÖ-0.6-0.8Time (nondimensionalised)-1Unsteady force on the flap0.00100.00050.0000-0.000500 5 10 15 20 25 30 35-0.2-0.0010´µÐÔÐÓÛÖ×ÙÖ-0.4-0.6-0.0015-0.8Time (nondimensionalised)ÓÖÚÐÙ×ÖØÒÓÒØÔÙÔÔÖÒÐÓÛÖ×ÙÖ×ºÙÐÖ×ÑÙÐØÓÒØÅ¼ºÒ ÙÖº½ÌÙÒ×ØÝÓÖÒÔÑÓØÓÒÛÒÚÒ×ÑÐÐÒØÐÔÖØÙÖØÓÒºÍÒ×ØÝ ´µÐÔÐÓÛÖ×ÙÖ-0.0020-1-4 -3 -2 -1 0 1 2 3 4Flap angle [degrees]ÝÒÑÔÖ××ÙÖ¾ºÈºNormalised unsteady force and flap motion10.80.60.40.2Normalised flap motionNormalised unsteady force
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Page 55 and 56: Flap´µFlapWingBlended width of th
Page 57 and 58: WingFlapFlap´µWingGapSheared cell
Page 59 and 60: Case 3: Mach 0.769, frequency 5 Hz.
Page 61 and 62: Rigid fuselageHierarchy level 1Wing
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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 149 and 150: Generalised coordinate (rudder mode
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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