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Сообщение от carsmaster
This is the reference realistic aerodynamic data of the aircraft.
** CyCritH_0 1.29 - Cy 1.29 lift (in English often Cl) in direct flight at a critical angle of attack
** CyCritL_0 -0.69 - Cy -0.69 lift (in English often Cl) in inverted flight at a critical angle of attack
In IL-2, often well-realistic reference data.
But sometimes the correct realistic data does not work well.
The flight model is not perfect in IL-2, often it is necessary to conduct experiments.
Example:
http://airfoiltools.com/airfoil/deta...rkyh-il#polars |
Ahhh so it takes the cross section of the wing. If the wing top / wing bottom are almost the same shape, the values should be closer to equal. Wing top / wing bottom, curved vs flat respectively, the greater the spread of the values. I understand now, thank you.