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

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׺żº¸ ʺÆÓº¿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×ÒÐҭԺżº¸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