Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Case 3: Mach 0.769, frequency 5 Hz.Case 3: Mach 0.769, frequency 5 Hz.Out of phase component of the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.005000 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1-0.005-0.005X/CX/C´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.01-0.01-0.015-0.015-0.02-0.02-0.025-0.025ÙÖº½¿Ì׿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ׺Å-0.03-0.03-0.035-0.035¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼Æ¸ÀÞº ´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.04-0.04Out of phase component of the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.0050.030.030.02FOF 5 Hz0.02FOF 10 HzGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised timeGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised time0.030.030.02FOF 15 Hz0.02FOF 20 HzGeneralised coordinate0.0100´µ-0.01-0.01ÙÖº½ÏÒÒÒÖ×ÔÓÒ×ØÓ«ÖÒØÔÖÕÙÒ׺ ´µ-0.02-0.02-0.03-0.030 50 100 150 200 250 300 3500 50 100 150 200 250Nondimensionalised timeNondimensionalised time½Generalised coordinate0.01
Generalised coordinate (wing bending mode)0.050.040.030.020.01timestep 0.14timestep 0.08timestep 0.04Generalised coordinate (wing bending mode)0.0040.0030.0020.001timestep 0.15timestep 0.0600-0.01-0.001´µØÓ½ÀÞÑÔÐØÙÒÖ××ÛØ-0.02Ö×ÒØÑ×ØÔº-0.002-0.03-0.003-0.04ÙÖº½ËÒ×ØÚØÝÓØÑÓÐÖ×ÔÓÒ×ØÓØØÑ×ØÔØØÖ×ÓÒÒÓØËË̸ ´µØÓ¾ÀÞÑÔÐØÙÖÑÒ×ÙÒ¹ ÒÛØÖ×ÒØÑ×ØÔº-0.05-0.0040 50 100 150 200 250 3000 50 100 150 200Nondimensionalised timeNondimensionalised time×½¸ÙÐÖ×ÑÙÐØÓÒº´µÄÓØÓÒÓÙÒ×ØÝÔÖ××ÙÖØÖÒ×ÙÖ׺ ÙÖº½ÄÓØÓÒÓÑ×ÙÖÑÒØÔÓÒØ×ÒØËËÌÜÔÖÑÒØ׺ ÒÑÓÖÑØÓÒº ´µÄÓØÓÒÓÓÔØÐØÖØ×ØÓÑ×ÙÖݹ¾
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- 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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- Page 77: Case 3: Mach 0.769, frequency 5 Hz.
- 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 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
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- Page 127 and 128: CFDNastranDynamic pressureBuzz regi
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., upper0.0150.010.005000 0.2 0.4 0.6 0.8 10 0.2 0.4 0.6 0.8 1-0.005-0.005X/CX/C´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.01-0.01-0.015-0.015-0.02-0.02-0.025-0.025ÙÖº½¿Ì׿ÙÒ×ØÝÔÚÐÙ×Ù×ÒÐÒÔÒÔÛØÔ׺Å-0.03-0.03-0.035-0.035¼º¸ÊºÆÓº¿ºÑÐÐÓÒ¸ÔÑÔÐØÙ¾¼Æ¸ÀÞº ´µÇÙØÓÔ×ÓÑÔÓÒÒØؼ±×ÔÒ-0.04-0.04Out <strong>of</strong> phase component <strong>of</strong> the unsteady Cp0.04 Blended, lower0.035Blended, upperGap, lower0.03Gap, upper0.025Expt., lower0.02Expt., upper0.0150.010.0050.030.030.02FOF 5 Hz0.02FOF 10 HzGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised timeGeneralised coordinate0.010´µ-0.01-0.02-0.030 100 200 300 400 500Nondimensionalised time0.030.030.02FOF 15 Hz0.02FOF 20 HzGeneralised coordinate0.0100´µ-0.01-0.01ÙÖº½ÏÒÒÒÖ×ÔÓÒ×ØÓ«ÖÒØÔÖÕÙÒ׺ ´µ-0.02-0.02-0.03-0.030 50 100 150 200 250 300 3500 50 100 150 200 250Nondimensionalised timeNondimensionalised time½Generalised coordinate0.01
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