Stepwise multiple regression results
| . | Beta coefficient . | P . | Adjusted R2 . |
|---|---|---|---|
| Lift coefficient | |||
| Angle of attack | |||
| Relative camber | |||
| Drag coefficient | 0.24 | ||
| Angle of attack | 0.528 | <0.001 | |
| Relative camber | –0.499 | 0.001 | |
| Lift-to-drag ratio | 0.411 | ||
| Angle of attack | –0.684 | <0.001 | |
| Relative camber | 0.618 | <0.001 | |
| Glide angle | 0.809 | ||
| Lift coefficient | –0.541 | <0.001 | |
| Drag coefficient | |||
| Wing loading | 1.233 | 0.001 | |
| Velocity | 0.793 | ||
| Lift coefficient | –0.684 | <0.001 | |
| Drag coefficient | –0.278 | 0.001 | |
| Wing loading | 1.449 | <0.001 |
| . | Beta coefficient . | P . | Adjusted R2 . |
|---|---|---|---|
| Lift coefficient | |||
| Angle of attack | |||
| Relative camber | |||
| Drag coefficient | 0.24 | ||
| Angle of attack | 0.528 | <0.001 | |
| Relative camber | –0.499 | 0.001 | |
| Lift-to-drag ratio | 0.411 | ||
| Angle of attack | –0.684 | <0.001 | |
| Relative camber | 0.618 | <0.001 | |
| Glide angle | 0.809 | ||
| Lift coefficient | –0.541 | <0.001 | |
| Drag coefficient | |||
| Wing loading | 1.233 | 0.001 | |
| Velocity | 0.793 | ||
| Lift coefficient | –0.684 | <0.001 | |
| Drag coefficient | –0.278 | 0.001 | |
| Wing loading | 1.449 | <0.001 |
Adjusted R2 is for the model as a whole
No reported value indicates that the covariate was excluded by the stepwise regression model