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| double | airfoil_Ia |
| double | airfoil_Ib |
| double | airfoil_Kaa |
| double | airfoil_Kah = 0.0 |
| double | airfoil_Kbb |
| double | airfoil_Kha = 0.0 |
| double | airfoil_Khh |
| double | airfoil_m |
| double | airfoil_Sa |
| double | airfoil_Sab |
| double | airfoil_Sb |
| double | amplitude0 = 0.0 |
| double | amplitude1 |
| double | amplitude2 |
| double | amplitude3 |
| double | angle = 0.0 |
| double | angularvelocity = 0.0 |
| double | cofgheight = 0.0 |
| int | COUPLED_MODEL = 10 |
| double | damping_aa |
| double | damping_ah = 0.0 |
| double | damping_bb |
| double | damping_ha = 0.0 |
| double | damping_hh |
| double | DragForce [HISTORY_LIFT] |
| double | FlapTorsionalMoment [HISTORY_LIFT] |
| int | FLUID_MODEL = 10 |
| double | force_lift |
| double | force_moment |
| double | frequency1 |
| double | frequency2 |
| double | frequency3 |
| double | LiftForce [HISTORY_LIFT] |
| int | NONLINEAR_STRUCTURE_MODEL = 1 |
| double | releasetime = 5.0 |
| double | releasetimesec = 0.01 |
| double | restartangle = 0.0 |
| double | restartflap = 0.0 |
| double | restarty = 0.0 |
| long | STATIONARY_ITER = 0 |
| int | STRUCTURE_MODEL = 10 |
| double | tail_angle = 0.0 |
| double | TorsionalMoment [HISTORY_LIFT] |
| double | velocity_tailangle = 0.0 |
| double | xhc |
| double | xlast [HISTORY_LIFT][10] |
| double | xmcenter |
| double | xRECENT [10] |
| double | xTAIL1 = 0.8 |
| double | xTAIL1orig = 0.8 |
| double | xTAIL2 = 0.81 |
| double | xTAIL2orig = 0.81 |
| double | yhc |
| double | ymcenter |
| double | yTAIL = 0.0 |
| double | yTAILorig = 0.0 |
| double | yvelocity = 0.0 |
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use geometrical nonlinearities |
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10 - fixed domain, 20 - prescribed motion (2 degrees of freedom,given ampl. & freq. ) 30 - aeroelastic model (2 degrees of freedom) |
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Fluid model (laminar/RANS+SA/RANS+SST) |
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fixed/prescribed motion/ode/Lame |
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number of stationary iterations |
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mean value for rotation |
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static components of aerod. forces |
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elastic axis recent location |
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elastic axis original location |
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flap params |
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flap params |
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1.4.6