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

Case 3: Mach 0.769, frequency 5 Hz.Case 3: Mach 0.769, frequency 5 Hz.Out of phase component of the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.005000 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1-0.005-0.005X/CX/C´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.01-0.01-0.015-0.015-0.02-0.02-0.025-0.025ÙÖº½¿Ì׿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒ­ÔÒ­ÔÛØÔ׺Å-0.03-0.03-0.035-0.035¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸­ÔÑÔÐØÙ¾¼Æ¸ÀÞº ´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.04-0.04Out of phase component of the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.0050.030.030.02FOF 5 Hz0.02FOF 10 HzGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised timeGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised time0.030.030.02FOF 15 Hz0.02FOF 20 HzGeneralised coordinate0.0100´µ-0.01-0.01ÙÖº½ÏÒÒÒÖ×ÔÓÒ×ØÓ«ÖÒØ­ÔÖÕÙÒ׺ ´µ-0.02-0.02-0.03-0.030 50 100 150 200 250 300 3500 50 100 150 200 250Nondimensionalised timeNondimensionalised time½Generalised coordinate0.01