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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15Flap <strong>with</strong> gapsBlended flap30Flap <strong>with</strong> gapsBlended flap1020Flap angle [degrees]50-5-10ÝÒÑÔÖ××ÙÖ¾ºÈ ´µÙÐÖÐÙÐØÓҸżº¸¼ºÒ-10-20ÙÖ¿º¾½ÐÔÖ×ÔÓÒ×ÓÐÒÒÖÔ×Ø«ÖÒØÅÒÙÑÖ×ÛØÐÒÒ ´µÙÐÖÐÙÐØÓҸżº¸¼ºÒ ÝÒÑÔÖ××ÙÖ¾ºÈ-15-300 20 40 60 80 1000 20 40 60 80 100Nondimensionalised timeNondimensionalised timeÔÖÑØÖÓ½¼¼Flap angle [degrees]100Case 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×ÓÑÔÓÒÒØؼ±×ÔÒ-0.1-0.1ÙÖ¿º¾¾Ì׿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ׺Å-0.15-0.15¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼Æ¸ÇÀÞº ´µÁÒ¹Ô×ÓÑÔÓÒÒØؼ±×ÔÒ-0.2-0.2½In-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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