Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft
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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 93 and 94: 15Flap with gapsBlended flap30Flap
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- 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 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
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