546
edits
Howto:Make a helicopter: Difference between revisions
Jump to navigation
Jump to search
m
→typo
m (→typo) |
|||
| Line 60: | Line 60: | ||
* '''maxcyclicail:''' The maximum of the cyclic incidence in degree for the aileron like function | * '''maxcyclicail:''' The maximum of the cyclic incidence in degree for the aileron like function | ||
* '''mincyclicail:''' The minimum of the cyclic incidence in degree for the aileron like function | * '''mincyclicail:''' The minimum of the cyclic incidence in degree for the aileron like function | ||
* '''airfoil-incidence-no-lift:''' non symmetric airfoils produces lift with no incidence.<br /> This | * '''airfoil-incidence-no-lift:''' non symmetric airfoils produces lift with no incidence.<br /> This is the incidence, where the airfoil is producing no lift. Zero for symmetrical airfoils (default) | ||
* '''incidence-stall-zero-speed:''' | * '''incidence-stall-zero-speed:''' | ||
* '''incidence-stall-half-sonic-speed:''' the stall incidence is a function of the speed.<br /> I found some measured data, where this is linear over a wide range of speed. Of course the linear region ends at higher speeds than zero, but just extrapolate the linear behavior to zero. | * '''incidence-stall-half-sonic-speed:''' the stall incidence is a function of the speed.<br /> I found some measured data, where this is linear over a wide range of speed. Of course the linear region ends at higher speeds than zero, but just extrapolate the linear behavior to zero. | ||