| aircraft | |
| view | |
| diagram |
| kt | ||
| ° | ||
| 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 |