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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Case 3: Mach 0.769, frequency 5 Hz.Case 3: Mach 0.769, frequency 5 Hz.Out <strong>of</strong> phase component <strong>of</strong> the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.00500 0.2 0.4 0.6 0.8 1-0.005-0.005X/CX/C-0.01-0.01´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.015-0.015-0.02-0.02-0.025-0.025-0.03-0.03ÙÖ¿º¾¿Ì׿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ׺Å-0.035-0.035¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼Æ¸ÇÀÞº ´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.04-0.04ØÖÓÐ×ØÐÙÐØÓÒ׺ÁÒØÙÖÖÒØÛÓÖØÑÔÔÒ×ÓÒ×ÔÖÔÖÓ××Ò×ØÔ ÌÑÔÔÒÓØÖÓÝÒÑÖØÓØ×ØÖÙØÙÖÐÖ×ÓÒÓØÒØÖÐ×ØÔ×Ò ¿º ÅÙÐعÓÑÔÓÒÒØÌ×Ø×ÒجØÓÒÓØØÖÒÙÐÖÐÑÒØØÓÛ×ÙÖÖÓÝÒÑÔÓÒØ×ÒÓÖØÓ¸ ××ÑÐÓÖØÝÔÐÖÓÐ×ØÐÙÐØÓÒºÌÑÔÔÒÐÓÒجÙÖÒÚÓÐÚ×Ø ÓÖÔÖÓÖÑÒØÓÙÔÐÐÙÐØÓÒ׺ÙÖ¿º¾×ÓÛ×ØÚÖÓÙ×ÓÑÔÓÒÒØ×ØØÖÒØÐÙÐØÓÒÓØ×ØÒÓÔÓÒØÓÒØÐÓÛÖÖÖÝÙÓÑÔÓÒÒØÖÓÑ ØÒÖ×ØÔÓÒØÓÒÒÙÔÔÖÖÖݺÌ××ÛÖØØÒÓÛÒÒÑÔÔÒ¬ÐÛ×Ù× ÓÖØÎÌÒÓÑÔÓÒÒØÐÒÒ×Ñ××ÖÒËØÓÒ׿ºÒ¿ººÇÒØ ÑÔÔÒ¬Ð×ÓØÒ¸ØØÖÒ×ÓÖÑØÓÒÒ×ØÓÚ×ÙÐÐÝÒ×ÔØÓÖÑÓÓØ ×ØÖÙØÙÖºÌ×ÒÓÒÝÓÖÒØ×ØÖÙØÙÖØÓ×ØØÐÐÝÓÖÑÒÑÓÛØÓÙØØÙÐÐÙÐØÓÒ׺ ØÙÐÐÝÔÖÓÖÑÒØÙÐÙÐØÓÒ׺Ì×ÐÙÐØÓÒ×ÓÒÓØÚÒÝÔÝ×ÐÑÒÒ ÜÔØÓÖÑÑÒØ×ÙÖÖØÖÒ×ÓÖÑØÓÒÓØÒÚÙÐÑÓ×Ô×ÙÖÒØØÖÖ¿ÐÚÐ×ÓÖÖݺ̬Ö×ØÐÚÐ×ØÙ×ÐØÓÛØÛÒ×Øغ ØÓÒÏÓÖ×ÓÔºÁØ×ÖÐØÚÐÝÓÑÔÐÜÓÑØÖÝÓÖÒÓÒÐÒÖÖÓÐ×ØÐÙÐØÓÒ×× ÌÒÖÄÖÖÖشĵØ×Ø××ÒÔØÖÓÑØÁÖÈÖ¹ÓÒÖÖÝÓÑÔÓÒÒغÌÔÝÐÓÒ×ØØØÓØÛÒ¸ÒØØÛÒ¹ÔÝÐÓÒÙÒØÓÒ ØÓÖÑØÓÒ×ÙØÓØÛÒÒÒØÔÝÐÓÒ×Ð×׬×ØØÖÖÖÝ ÀÖØÓÖÑØÓÒÓØÛÒÖÓÓØÔÒ×ÓÒØÙ×иÒØ×Ð×׬ÒØÓ×¹ØÓÒØØÙÒØÓÒØÛÒØÒÐÐÒØÔÝÐÓÒ×ÙØÓØÒÐÐÒÒÓØØ ÔÝÐÓÒºÅÓÖÓÚÖ×ØÒÒ×Ø×ØÒÖÓÑØÙ×ÐØÒÙÒÓØÙ×ÐÓÒ ÓÑÔÓÒÒغÌÒÒÒÐÐÓÛÚÖ×Ð×׬ÒØÓ×ÓÒÐÚÐÓÑÔÓÒÒØ×ÒØØÒÐÐ×ÒÐÐÓÒÓÙÒØÓØÜÔÓÒÒØÐÐÒÒÔÖÑØÖ×ÖÒËØÓÒ ¿ººÙÖ¿º¾×ÓÛ×ØÖÖÐÐ×׬ØÓÒÓØ×ØÖÙØÙÖÐÓÑÔÓÒÒØ×ÓØÖÖغ ¾Out <strong>of</strong> phase component <strong>of</strong> the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.00500 0.2 0.4 0.6 0.8 1
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