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See:
Description
| Class Summary | |
|---|---|
| CustomAeroCoeffByAltitude | Aerodynamic coefficient function of the spacecraft altitude. |
| CustomAeroCoeffByAoA | Aerodynamic coefficient function of the spacecraft angle of attack. |
| CustomAeroCoeffByAoAAndMach | Aerodynamic coefficient as a function of two variables: the angle of attack and the mach number. |
| CustomAeroCoeffByMach | Aerodynamic coefficient as a function of the mach number. |
| CustomAeroCoeffByOneVarAbstract | Defines a function with one variable from an array of x and y values. |
Package containing some objects related to vehicle aerodynamic coefficients functions intended to be added to PATRIUS. There should not be any genopus dependancy inside this package.
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