| aircraft | |
| view | |
| diagram |
| kt | ||
| ° | ||
| X | X | X | ||
thrust |
||||
wing lift |
||||
elev lift |
||||
wing drag |
||||
elev drag |
||||
total lift |
||||
total drag |
||||
wing l&d |
||||
elev l&d |
||||
weight |
||||
ground |
||||
resultant |
| kgf | hp | ||
prop lift |
|||
prop drag |
|||
thrust |
|||
prop force |
|||
total force |
|||
shaft force |
|||
| kt | |||
rot. flow |
|||
induced rot. flow |
|||
total rot. flow |
|||
axial flow |
|||
induced axial flow |
|||
total axial flow |
|||
total flow |
|||
| 0 | ft |
| 0 | ft/min |
| 0.0 | g |
| flaps |