Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
ÙÖº×ÓÛ×ØÐÒÒØÖÐÒÖÖ×ÒØØÓÒÓØÜØÖÒØÖÑØÖ׺ÌÓÑÔÓÒÒØ×ÖØØØÓØÖÖ×ÔØÚÔÖÒØÓÑØÖÝØÖÓÙ×ÔÖÒØØÑÒØ×´Ä˾ÒØÖ×ÒÆ×ØÖÒµºÌ×ÔÖÓÚ××ÓÑÓÒØÖÓÐÓÚÖØÑÓÐÖÕÙÒ×ÓØÒÚÙÐÓÑÔÓÒÒØ׺ÀÒØÓÒØÖÓÐ×ÙÖ×ÖØØØÓØÛÒÒØÚÖØЬÒØÖÓÙ×Ø«×ÔÖÒ׸ÒØÛÒÒ¬ÒØÑ×ÐÚ×ÖØØØÓØÙ×ÐØÖÓÙ×ÔÖÒ׺Ìк½Ú×Ø×ÔÖÒ×Ø«Ò××ÚÐÙ×Ó«ÖÒØÓÑÔÓÒÒØ׺ÌÔØÒÜ×ÓØ×ØÖÙØÙÖÐÑÓÐ×ØݹÜ×ÖºÓÖÐÙÐØÓÒ×ØÞ¹Ü×ÓÖÑ×ØÔØÒÜ×ÒÒØ×ØÖÙØÙÖÐÑÓÐÜ×ÖØÖÒ×ÓÖÑÐØÖØÓÓÒÓÖÑØÓÖÕÙÖÑÒØ׺ÌÓÒØÖÓÐ×ÙÖ×ÒØÖÑ×××ÖÒÐÙÒØ×ØÖÙØÙÖÐÑÓÐÙØØÖÖ×ÔÓÒ××ÒÓØÓÒ×ÖÒØÖÓÐ×ØÐÙÐØÓÒ׺ÀÒÐØÓÙØÔÖ×ÒÓÓÒØÖÓÐ×ÙÖ׫Ø×ØÛÒÑÓ׸ØÓÖÑØÓÒÓØÓÒØÖÓÐ×ÙÖ×ØÑ×ÐÚ××ÒÓØÒÐÙÒØÛÒÐÓÒÒÐÝ×׺Ìк¾Ú×ØÖÕÙÒ×Ò×ÖÔØÓÒÓجÖ×ؽ¼ÑÓ׺XYZ74000XYZ74600XYZ74800XYZ74900XYZ75000XYZ76000XYZ77000XYZ78000XYZ79000XYZXYZÙÖº¾ÀÛ×ØÖÙØÙÖÐÑÓкº¾º¿Ê×ÙÐØ×Ö×ØÝ×ØØÐÙÐØÓÒÛ×Ù×ØÓÒØÐ×Ø×ØØÖÓÐ×ØÐÙÐØÓÒ¸ÛÒØÓÒÚÖÖÔÐÝ×ÒÚÖÝ×ÑÐÐÓÖÑØÓÒÛ×Ó×ÖÚºÌÒ¸ÒÓÒÞÖÓÒÖÐ×ÚÐÓØÝÓÖجÖ×ØÑÓÛ××ØÒØØÑÑÖÒÐÙÐØÓÒ××ØÖغÌÖ×ÔÓÒ×ÓÖ«ÖÒØÚÐÙ×ÓÝÒÑÔÖ××ÙÖÛ×ÓØÒÒØÖ×ÔØÛ×ØÐØÝ×ÐÓ×ØÛ×ÒÖÖÖÓÑØÖÓÛØÓÖÝÓØ×Ö×ÔÓÒ×׺ËØÖÙØÙÖÐÑÔÒÚÐÙÓ¼±Û×Ù×ÒØÆ×ØÖÒÒØÐÙÐØÓÒ׺ØÐØÑ×ØÔÓÒÚÖÒ×ØÙÝÛ×ÖÖÓÙØÒÒÐЫÖÒ×ØÛÒÙ×Ò¼ØÑ×ØÔ×ÔÖÙØØÖÝÐÒ×ÑÐÐÖØÑ×ØÔ×ÛÖÓ×ÖÚÓÒÐÐÖ×ÒØÐÐÅÒÙÑÖ׺ÀÒ¸Ø×ØÑ×ØÔÛ×½¼
ÙÖº¿Ù×ÐÜÙÖÐÜ×ÛØØØÖÖ×ÓÑÔÓÒÒØ ÏÒ ´Æ»Ñµ´Æ»Ñµ ÌÜ ÌÝ ´Æ»Ñµ ÌÞ ´Æѻֵ´Æѻֵ´Æѻֵ ÊÜ Êݵ ÊÞ Å××ÌÐ ½º½¢½¼ ¢½¼ ¢½¼ ¾¢½¼ º¢½¼ ¢½¼ ¾¢½¼ ¼º¿¾½ º ´ÃµÊÙÖ Ò ½¢½¼½¾ ½¢½¼½¾ ½º¿¢½¼¿ ½¢½¼½¾ ¿¿º½½ÐÖÓÒ ÐÔ ½¿½º¾¢½¼¿ ¾º¢½¼¿ ½º º½ º¾Ù×Ð Ìк½ÎÐÙ×Ó×ÔÖÒÓÒ×ØÒØ×ÒÑ×××ÓÓÑÔÓÒÒØ ¹ ¹ ¹ ¹ ¹ ¹ ¾¼½º½½¼
- Page 65 and 66: ÙÖº½ÌÌÛÒØÙÒÒÐÑÓÐÛ
- Page 67 and 68: º¾º¾ÌÆÄËËÌÖÖÓÛÏÒ Ù
- Page 69 and 70: WingDeflected flapØØØÖÙÖÕÙ
- Page 71 and 72: ÐÒ¸ØÛÒØÔÒÐ×ÓÖÓÙÒØ
- Page 73 and 74: ÑÓÖ×¾ØØÖ×ÓÒÒØÖÕÙÒ
- Page 75 and 76: ´µËØÖÙØÙÖÐÑÓÐY:´µÅ
- 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
- Page 87 and 88: ÓÒØÖÓÐËÙÖÁÒ×ØÐØÝ Ô
- Page 89 and 90: ÅÓ ÏÒÒÒ ÐÔÇ×ÐÐØÓÒ ½
- Page 91 and 92: 3020∆ t = 0.1∆ t = 0.05∆ t =
- Page 93 and 94: 15Flap with gapsBlended flap30Flap
- Page 95 and 96: 0.020.020.0150.015Generalised Coord
- Page 97 and 98: 0.020.02Generalised Coordinate0.010
- Page 99 and 100: 10.90.00250.8Generalised Coordinate
- Page 101 and 102: 4040Initial grid velocity 0.02Initi
- Page 103 and 104: Unsteady force on the flap0.00100.0
- Page 105 and 106: Unsteady force on the flap (nondime
- Page 107 and 108: 20152010Flap angle [degrees]50-5-10
- Page 109 and 110: ÌÖ×ØÖÑÚÐÓØÝ×½¾Ñ»×
- Page 111 and 112: ×ØÖÙÖÕÙÒÝÚÒݾ ÛÖØ×
- Page 113 and 114: ÌÀÛÖÖؽ ÔØÖº½ ÁØ×Ò
- Page 115: ÐÙÐØÓÒ¸ØØÑ×ÛÖ×ÓÒ×
- Page 119 and 120: ÖÕÙÒÝÀÞ℄ ½¾º¾ ½º¾
- Page 121 and 122: × ÓÑØÔ ÏÒÛØÔ¼Æ ½¾
- Page 123 and 124: ×ÐÐÓÛº ÚØÝ×ÓØÔÐÒ×
- Page 125 and 126: ÅÓ½½¾º ÅÓ¾¿º ÖÕÙÒÝ
- Page 127 and 128: CFDNastranDynamic pressureBuzz regi
- Page 129 and 130: ÙÖº½ØØÓÛÐÐÐÓÒØÔ
- Page 131 and 132: ÖÖظÒÒØ×ÖÙ×ÓÖØÐÙÐ
- Page 133 and 134: The Hawk Body-Fin-Wing-Rudder CaseO
- Page 135 and 136: ÅÖÖÓÖÒÓÅÓ× ÌØÖØÑÒØ
- Page 137 and 138: ×½½½Æ ×¾ ÁÒÒÅÒÙÑÖ ¼
- Page 139 and 140: ÓÖØÖ××ÓÒÖ×ÒÓÑØÖÓÑ
- Page 141 and 142: Spanwise locations on the fin of th
- Page 143 and 144: -Cp on the fin at Y=2.4 MetresBAE-F
- Page 145 and 146: B-F-R Case, Euler Simulation, Mach
- Page 147 and 148: CFDLinearB-F-R (Onset of buzz)B-F-R
- Page 149 and 150: Generalised coordinate (rudder mode
- Page 151 and 152: ÛÖÒÓØÔÖØÝØÙÐÖÕÙØÓ
- Page 153 and 154: ÓÒØÖÓÐÐÛÒÓÖÑØÓÒ×Ò
- Page 155 and 156: ½℄ÆËÙÓÑÑØØÓÒÎÖØÓÒ
- Page 157 and 158: ℄úÊÓÙҸźÖÒ̺ÓÖØ
- Page 159 and 160: ℄ºÃÖÐ××ÓÒÒºÏÒÞÐк
ÙÖº¿Ù×ÐÜÙÖÐÜ×ÛØØØÖÖ×ÓÑÔÓÒÒØ ÏÒ ´Æ»Ñµ´Æ»Ñµ ÌÜ ÌÝ ´Æ»Ñµ ÌÞ ´Æѻֵ´Æѻֵ´Æѻֵ ÊÜ Êݵ ÊÞ Å××ÌÐ ½º½¢½¼ ¢½¼ ¢½¼ ¾¢½¼ º¢½¼ ¢½¼ ¾¢½¼ ¼º¿¾½ º ´ÃµÊÙÖ Ò ½¢½¼½¾ ½¢½¼½¾ ½º¿¢½¼¿ ½¢½¼½¾ ¿¿º½½ÐÖÓÒ ÐÔ ½¿½º¾¢½¼¿ ¾º¢½¼¿ ½º º½ º¾Ù×Ð Ìк½ÎÐÙ×Ó×ÔÖÒÓÒ×ØÒØ×ÒÑ×××ÓÓÑÔÓÒÒØ ¹ ¹ ¹ ¹ ¹ ¹ ¾¼½º½½¼