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

More documents

Recommendations

Info

ÒÙÑÖ×ºÀÓÛÚÖÙÞÞÒ×ØÐØÝÒÔÖÙØØÖÒ×ØÐØÝØØÖÒ×ÓÒÅÒÙÑÖ× ×ÒÙÞÞÓÙÖ×ÚÒØÐÓÛÚÐÙ×ÓÝÒÑÔÖ××ÙÖºÒ×ØÐØ×ºØÐÓÛØÙÖ×ÒØ×ØÖÙØÙÖÐÓÖÑØÓÒ×ÒÜØÖØØÒÝÑÓ¹ Ð×ØÒÐÝ×××ØÔÐØÝØÓÙÖØÐÝÒØÝÒÙÒÖ×ØÒØÔÝ××ÒØ ÁØ××ÓÛÒÝÐÐØ××ØØÚÒÒÐÝ×ÒØ×ÛÓÖØØØÑÑÖÒÖÓ¹ÑÒØÓØÑºÅÓÖÓÚÖÒØ¬ØÓÒÓÒ×ØÐØ×ÐÙÞÞÛÖÝÓÒØÑÓÐÐÒ ÔÐØ×ÓÐÒÖÑØÓ×ÒÓÒÙÖØÐÝºÀÓÛÚÖÙØÓØÐÓÒÖÙÒØÑ×¸ØÑ ÒÙ×ØÖÝºÌÙ×ÓÑÙ×ØØÖØØØÆÙÐØÓÛÖÑ×ÓÖºØÖÒ×ÓÒÅ ÑÖÒÑØÓ×ÒÒÓØÖÔÐÑÒØÓÖÐÒÖÑØÓ×ØØÖÙÖÖÒØÐÝÙ×ÒØ ÒÙÑÖ×´ÙÞÞµÒÒÐÓØØÓÛ×´Ù«ØµºÊ×ÖÈÖØÒÖ×Ô×ÈÍÅÊÈ×ÔÓÒ×ÓÖÛÓÖÒÓØ×Ù××ÖÐÖÒØØ×××Ò º ÇÒÓØÓÙØÓÑ×ÓØÈÖØÒÖ×ÔÒÍÒ×ØÝÅÓÐÐÒÓÖÓÝÒÑ×¹ÒÒ ÒÁÒÙ×ØÖÝØÐÓ×ÓÐÐÓÖØÓÒÛØØÒÒÖ×ØËËÌÅËÓÖØÖÓÐ×Ø×ÑÙÐØÓÒ×ÓÒ ØÀÛÖÖØºËØÖÙØÙÖÐÑÓÐ×Ù×ÓÖÙØØÖÐÖÒÛÖÖÐ×ÝØÓÑÔÒÝ ØÖÒÒØÙ×ÓØÓÓÖÖÓÐ×ØØÝºÐÖÖÝÓ×××Ò×ØÙÔØØ ÓÖÙ×ÒØ×ÖÓÐ×ØÒÐÝ××ºÁÒØÙÖÒØÒÒÖ×ÖÓÑØÓÑÔÒÝÛÖ ËËÌÅËÐØÝÒÖÓÙºÌÓÙÔÐ××ÚÒ×ØÙÔÒÑÒÒÖØØ ÒÝÒ×ÒØ×ØÖÙØÙÖÐÑÓÐÒ×ÐÝÖÐ×ÒØÖÓÐ×ØÐÙÐØÓÒ×ÛØ ÑÒÑÐÔÖÔÖÓ××ÒÓÒÐÓØÒÒÖ×ºÌ×××Ò¬ÒØ×ØÔÒÒÖ×ÒØ ÓÒ¬ÒÒ××ÑÙÐØÓÒ×ØÔÖÓÙØÓÒÐÚÐÒÛÐÐÒÓÙÖØÙ×ÓÓÖ ÒÚ×ØØÓÒÓÙØÙÖÖÓÐ×ØÔÖÓÐÑ×ÛÒÒØÝÖ×º º ÓÒØÖÓÐ×ÙÖ×Ú×ÓÑÖÔÐÝÙÐØÒÙØÓØÑÒÙØÙÖÒÐÑØØÓÒ×ºÌ×ØÒÖ× ÓÒØÖÓÐ×ÙÖÖÔÐÝ×ÓÒÓØÑÔÓÖØÒØ××Ù×ÒØÖÖØÒÙ×ØÖÝºÐÑÓ×ØÐÐ ÙØÙÖÏÓÖÔÖ×ÖÝØÚØÓÒÙØÓÖØ×ÖÆÙÐØØÓÓÒ¬ÖÑÛØºÁØ×ÐØØØØ×ÖÙÐØÓÒ× ÓÙÐÖÐÜØÖ×ÑÓÖÙÒÖ×ØÒÒÓØÖÓÐ×ØÖ×ÔÓÒ×ÙØÓÖÔÐÝº ×ÒÐÝ×××ÒÜÐÐÒØØÓÓÐØÓ×ØÙÝØ×ÔÒÓÑÒÓÒºÓÖØÖÓÐ×ØØÓÓÐÙ×ÒÓØÙÖÖÒØÛÓÖÛ×ÐÖÝ×ØÐ×ØÔÐØÝÓØÓØÓØÖØÓÒØÖÓÐ ÐÒÖÑÓÐÅ×ÓÐÚÖØØ×ÓÙÔÐØÓØÙ×ÓÐÚÖºÌ×ÒÒÒØÖ×ØÒÜØÒ×ÓÒ ØÙÖÖÒØÛÓÖØÒÚÓÐÚ×ÑÔÐÑÒØÒØÒÕÙØÓØÖØØÖÔÐÝÒÓÒÐÒÖØÝÒØ×ÙÖÒ×ØÐØÝÓØÒÒ¬ÐÖÓÝÒÑÒÐÒÓØÛÒº×ØÖÓÐ×ØÓÖÑØÓÒÒ×ØÓ ØÐÓÖÒÒ¬Ò×ÓÒØÖÓÐÐÖÓÐ×ØÓÖÑØÓÒÓØÛÒ×ØÖÙØÙÖÒÓÖÖØÓ ÁÒÖÒØÝÖ×ÖÓÐ×ØØÐÓÖÒÓÖÖØÛÒ×ÚÓÑÔÓÔÙÐÖºÖÓÐ×ØÓÒØÖÓÐÐØÖÕÙÖ×ËÑÖØÅØÖÐØÙØÓÖ×ØØÒÓÖÑÓÖÑÓÖÔØÛÒ×Ô× ÖÕÙÖºÌØÙØÒÑÒ×ÑÒÓ×ØÐÝÒÓÖÑÓÐ×ÙÐØØÛÓÙÐÐÔÙÐ ÖÓÝÒÑÔÖÓÖÑÒºÌÑÑÖÒ×ÑÙÐØÓÒ×ÒÔÖÓÚÔÖØÓÒ×ÓÖØ×º ØÓÚÒÓØÓÖÑ×ÔÒØÖØÓÓÖÑØÓÒØØÛÓÙÐÚÓÔØÑÙÑ½
ÓÒØÖÓÐÐÛÒÓÖÑØÓÒ×ÒÓÖÓ×ÐÐØÓÒ×ÖÔÓ××Ð××ÓÛÒÒØÓÖÔ ×ØÙÝÖÐÖºÌ×ØÖÙØÙÖÐÑÓÐÒØÙÒÓÑÔÙØØÓÒÐÐÝØÓÔÖÓÚØ×ØÖ×ÙÐØ×ØÓÒ×ÓÒÒÖÖØÒÑÒÓÙÚÖºÅÐØÖÝÖÖØ×ÒÙÒÖØÖÔÑÒÓÙÚÖ×Ö×ÙÐØÒ ÒØ×ÒÙ×ØÓÙØÑÒÙØÙÖÓØÖÐÛÒºÒÐÖÖÓÝÒÑÒÐÓ×ÓÒØÛÒ×ºÌ×ÒÙ×ÐÖÓÖÑØÓÒ×ÓØÛÒ×º ÒÒØÖ×ØÒÔÔÐØÓÒÓØØÑÑÖÒ×ÑÙÐØÓÒ×ÖØÐÓ×ÒÓÖÑ¹ÑÒÓÙÚÖÒÐÔÒØ×ÒÓØÛÒ×ÒÓÖÐÙÐØÒØÓÔÖØÓÒÐÐÑØ×ÓØ ÓÑÔÙØØÓÒÐÔÐØÝÓÔÖØÒØÐÓ×ÒØÓÖÑØÓÒ×ÓÒÒÖÖØÒ ÖÖØºÌ×ÒÙØÙÖÜØÒ×ÓÒÓØÙÖÖÒØÛÓÖº½
Page 1 and 2:
ÖÓÐ×ØÒÐÝ××ÓÖÖØ ÛØÓ
Page 3 and 4:
×ØÖØÒØ×Ò×ØºÍÒØÐØÚ
Page 5 and 6:
ÓÒØÒØ×½ÁÒØÖÓÙØÓÒ ½
Page 7 and 8:
º¿ÄÑØØÓÒÓÄÒÖÖÓÝÒÑ
Page 9 and 10:
ÔÔÐÖÓÝÒÑÓÖ×ºÌÖÓÝÒ
Page 11 and 12:
ÒÚÓÐÚØÖÒ×ÓÒÓÒØÖÓÐ
Page 13 and 14:
ÌÑÓØÚØÓÒÓÖØÙÖÖÒØÛ
Page 15 and 16:
ÓØÒ×ØÐØÝÓÙÒÖÝØØÖÒ
Page 17 and 18:
¾º¾º½ÆÓÒ¹ÑÒ×ÓÒÐÓÖ
Page 19 and 20:
ÒÐÐÝ¸ØÐÑÒÖÚ×Ó×ØÝ×
Page 21 and 22:
ÛÖ½Â ÏÏÂ ½Â Ü·Ý·ÞÀ¡
Page 23 and 24:
ÇÒØÓØÖÒ¸ØÖØÚØÒÕÙ×
Page 25 and 26:
AB×ÖÓÙØÓÙØÒ×ØÔ½ºÒÐ
Page 27 and 28:
Ì×ÖÐÙÐØ× ÛÖ×½´µ×¾´
Page 29 and 30:
ÒÖÐÙÐØÖÓÑ ÌÙÒØÓÒ×Ò
Page 31 and 32:
Å××ÒÖÐ×ØÓÒ×ÔÖÓÖÑØ
Page 33 and 34:
ÌÖÒ×ÓÖÑØÓÒÅØÓÓÐÓÝ
Page 35 and 36:
ÙÖ¿º¾ÖÐÓÔÓÒØ×ÖÐÝÖ
Page 37 and 38:
¿º¿ ×Ù×ØÓØÖÒ×ÖÓÖ×º
Page 39 and 40:
Fluid Grid Node−1,1η1,1(x,y)(ξ,
Page 41 and 42:
ÕÙØÓÒ¿º¾ÒÙ×ÓÒÐÝØÒ
Page 43 and 44:
ÁØÛ×ÓÙÒÒ℄ØØØÐÒÖ×Ø
Page 45 and 46:
BBPÙÖ¿ºËÖ××ÛÒÔÐÒÔÖÓ
Page 47 and 48:
X1s,kPurely translated fictitious p
Page 49 and 50:
Structural ComponentLevel 1 Mapping
Page 51 and 52:
Control surface treatmentsBlended e
Page 53 and 54:
¿ººÔÐÓ× ÒÓØÖÓÔØÓÒÓ
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
Page 63 and 64:
ÎÐØÓÒÓÖÓÖÐÔÅÓØÓÒ×
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: ×ØÖÙÖÕÙÒÝÚÒÝ¾ ÛÖØ×
Page 113 and 114: ÌÀÛÖÖØ½ ÔØÖº½ ÁØ×Ò
Page 115 and 116: ÐÙÐØÓÒ¸ØØÑ×ÛÖ×ÓÒ×
Page 117 and 118: ÙÖº¿Ù×ÐÜÙÖÐÜ×ÛØØ
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: ÖÖØ¸ÒÒØ×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: ÛÖÒÓØÔÖØÝØÙÐÖÕÙØÓ
Page 155 and 156: ½℄ÆËÙÓÑÑØØÓÒÎÖØÓÒ
Page 157 and 158: ℄ÃºÊÓÙÒ¸ÅºÖÒÌºÓÖØ
Page 159 and 160: ℄ºÃÖÐ××ÓÒÒºÏÒÞÐÐº
show all

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

Create successful ePaper yourself

Delete template?

Save as template?