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

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Page 11 and 12: ÒÚÓÐÚØÖÒ×ÓÒÓÒØÖÓÐ
Page 13: ÌÑÓØÚØÓÒÓÖØÙÖÖÒØÛ
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
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º¾º¾ÌÆÄËËÌÖÖÓÛÏÒ Ù
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WingDeflected flapØØØÖÙÖÕÙ
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ÑÓÖ×¾ØØÖ×ÓÒÒØÖÕÙÒ
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´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
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ÓÒØÖÓÐËÙÖÁÒ×ØÐØÝ Ô
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ÅÓ ÏÒÒÒ ÐÔÇ×ÐÐØÓÒ ½
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3020∆ t = 0.1∆ t = 0.05∆ t =
Page 93 and 94:
15Flap with gapsBlended flap30Flap
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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
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20152010Flap angle [degrees]50-5-10
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CFDNastranDynamic pressureBuzz regi
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ÖÖØ¸ÒÒØ×ÖÙ×ÓÖØÐÙÐ
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The Hawk Body-Fin-Wing-Rudder CaseO
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×½½½Æ ×¾ ÁÒÒÅÒÙÑÖ ¼
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Spanwise locations on the fin of th
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-Cp on the fin at Y=2.4 MetresBAE-F
Page 145 and 146:
B-F-R Case, Euler Simulation, Mach
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CFDLinearB-F-R (Onset of buzz)B-F-R
Page 149 and 150:
Generalised coordinate (rudder mode
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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