|
Aero Class Table
|
Display general information about the available Aero Classes. | Setting | Description |
|---|
| Group, Aero |
Group and name of Aero Class |
| RefCS: |
Cross section related to the Aero Class for calculation with CFD module |
| Data, Sym |
Type of data and flag indicating if coefficients for - directions can be deduced from those of + directions
- Single Values: Only one coefficient and derivate is given per main direction
- Table: Several values can be given for each main direction
|
| FactorX, FactorY, FactorZ |
Additional factors for steady state coefficients |
| DragX, FIDx |
Drag coefficient for longitudinal wind and normalization length |
|
|
Buttons
|
|
|
Steady State Coefficient Table
|
Display and modify steady state coefficients of selected Aero Class. | Setting | Description |
|---|
| Recalc |
Indicates if the line will be recalculated when calling the next Action>Aero Note: The recalculation state can be changed by pressing the <C> key
|
| Direction, Angle |
Main direction and angle of table entry |
| Cd, Cd', Cl, Cl', Cm, Cm' |
Dimensionless drag-, lift- and moment coefficient and derivate with respect to angle |
| A, St |
Dimensionless amplitude and frequency (Strouhal number) of vortex shedding |
| Norm |
Normalization length for C, C', A and St, respectively |
|
|
Buttons
|
|
