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

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Case 1 : Incidence -4.02, Mach 0.769Case 1 : Incidence -4.02, Mach 0.7691.5 Blend, lowerBlended, upperGap, lowerGap, upper1Expt., lowerExpt., upper1.5 Blended, lowerBlended, upperGap, lowerGap, upper1Expt., lowerExpt., upper0.50.5-Cp0-0.5´µ¼±×ÔÒ-Cp0-1-1ÙÖºÌ×½×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ×ºÅ¼º¸ ÊºÆÓº¿ºÑÐÐÓÒ¸« ¼¾Æ0 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1Unit chordUnit chord-0.5´µ¼±×ÔÒCase 2: 5 degrees flap deflection, Mach 0.769Case 2: 5 degrees flap deflection, Mach 0.7691Blended, lowerBlended, upperExpt., lowerExpt., upper1Blended, lowerBlended, upperExpt., lowerExpt., upper0.50.5-Cp-Cp00´µ¼±×ÔÒ-0.5-0.5ÙÖº½¼Ì×¾×ØÝÔÚÐÙ×Ù×ÒÐÒÔºÅ¼º¸ÊºÆÓº¿º ÑÐÐÓÒ¸ÔÒÐ¼Æ ´µ¼±×ÔÒ0 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1Unit chordUnit chord
Case 3: Mach 0.769, frequency 5 Hz.Case 3: Mach 0.769, frequency 5 Hz.1Blended, lowerBlended, upperGap, lowerGap, upperExpt., lowerExpt., upper1Blended, lowerBlended, upperGap, lowerGap, upperExpt., lowerExpt., upper0.50.5-Cp-Cp00´µ¼±×ÔÒ-0.5-0.5ÙÖº½½Ì×¿ÑÒÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ×ºÅ¼º¸ ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼¾Æ ´µ¼±×ÔÒ0 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1X/CX/CCase 3: Mach 0.769, frequency 5 Hz.Case 3: Mach 0.769, frequency 5 Hz.In-phase component <strong>of</strong> the unsteady Cp0.2 Blended, lowerBlended, upperGap, lower0.15Gap, upperExpt., lower0.1Expt., upper0.0500 0.2 0.4 0.6 0.8 1X/CX/C-0.05-0.05´µÁÒ¹Ô×ÓÑÔÓÒÒØØ¼±×ÔÒ-0.1-0.1ÙÖº½¾Ì×¿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ×ºÅ-0.15-0.15¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼Æ¸ÀÞº ´µÁÒ¹Ô×ÓÑÔÓÒÒØØ¼±×ÔÒ-0.2-0.2¼In-phase component <strong>of</strong> the unsteady Cp0.2 Blended, lowerBlended, upperGap, lower0.15Gap, upperExpt., lower0.1Expt., upper0.0500 0.2 0.4 0.6 0.8 1
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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 103 and 104: Unsteady force on the flap0.00100.0
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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