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

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CP0.3248150.2683330.2118520.155370.09888890.0424074-0.0140741-0.0705556-0.127037-0.183519-0.24CP0.3240740.2666670.2092590.1518520.09444440.037037-0.0203704-0.0777778-0.135185-0.192593-0.25ÙÖºÌØÛÓØÝÔ×ÓÑÓÐÐÒÓØÔ×ÓÒØÌÒËËÌÛÒ×º ´µÔÓÒØÓÙÖ×ÓÒÐÒÔº ´µÔÓÒØÓÙÖ×ÓÚÖÔÛØÖ×ºÅÓ½¹Ö×ØÛÒÒÒ º ÎÌÅ¹ÇÖÒÐÅ¹ËØ«Ò ½½º¼ ÆØÙÖÐÖÕÙÒ×´ÀÞµ¹ ÅÓ¾¹Ö×ØÛÒØÛ×ØÒ ¹ ½º ½¾ºÅÓ¿¹ËÓÒÛÒÒÒº½º¾ ¼º¾º¼¼ ½º º¿¾ ¹ÝÒÑÓÖÑØÓÒÓØËËÌÓÑÔÖ×ÛÐÐÛØØÜÔÖÑÒØ×ØØÖ×ÓÒÒØÖÕÙÒÝ ÌÐº¿ÆØÙÖÐÖÕÙÒ×ÓØÜÔÖÑÒØÐÒÅÑÓÐ×ÓØËËÌÓÒ¬ÙÖØÓÒºÒÖ×ÓÒÐÓÑÔÖ×ÓÒÓÖÙÒ×ØÝÔÖ××ÙÖ×ØÖÙØÓÒÛ×ÓØÒÓÖÐÐÖÕÙÒ×º Î×ÓÙ×«Ø×ÛÖÓÙÒØÓÒÐÐÒÒÚ×ÔÖØÓÒ×ÛÖ×ÙÖØ×Ú×ÓÙ× ÓÖØ×ÛØ¼ÆÒÒºÁØ×ÓÒÐÙØØÙÐÖÕÙØÓÒ×ÒÙÖØÐÝÔÖØØ ÙÒ×ØÝÔÖ××ÙÖÓÖØÖÒ×ÓÒÅÒÙÑÖ×ÛÖØ×ÓÖÑÒ×ÛÐÐÓØÓÒØÖÓÐ ×ÙÖÒºÌ«ØÓÐÒÔ×ÓÒØÔÖØÓÒÓÔÖ××ÙÖ×ØÖÙØÓÒÒ ÓÖÑØÓÒÓÛÒÛ×ÓÙÒØÓÒ×Ò¬ÒØÛÒÓÑÔÖÛØÔ×ÛØÖ×ºÌ Å×ØÖÙØÙÖÐÑÓÐÛ××Ø«ÒØÓÐÐÓÛØÖ×ÓÒÒØÓØÔÐØÓ½ÀÞºÙØÙÖ ÛÓÖÓÙÐÒÐÙØÐÅÑÓÐØØØ×ÒØÓÓÙÒØØ×ØÖÙØÙÖÐÒÓÒÐÒÖØ×º
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Page 49 and 50: Structural ComponentLevel 1 Mapping
Page 51 and 52: Control surface treatmentsBlended e
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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 77 and 78: Case 3: Mach 0.769, frequency 5 Hz.
Page 79 and 80: Generalised coordinate (wing bendin
Page 81 and 82: Magnitude of unsteady pressure (non
Page 83 and 84: P: 0.6 0.666667 0.733333 0.8 0.8666
Page 85 and 86: Magnitude of unsteady pressure (non
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Page 97 and 98: 0.020.02Generalised Coordinate0.010
Page 99 and 100: 10.90.00250.8Generalised Coordinate
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Page 103 and 104: Unsteady force on the flap0.00100.0
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B-F-R Case, Euler Simulation, Mach
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CFDLinearB-F-R (Onset of buzz)B-F-R
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Generalised coordinate (rudder mode
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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