Please explain the forces acting on the airplane when applying power in a conventional piston engined aircraft with a traction engine installation Vs the configuration with a pusher prop on an engine mounted behind the vertical axis.
Please explain the forces acting on the airplane when applying power in a conventional piston engined aircraft with a traction engine installation Vs the configuration with a pusher prop on an engine mounted behind the vertical axis.
The following terms have been auto-detected the question above and any answers or discussion provided. Click on a term to see its definition from the Dauntless Aviation JargonBuster Glossary.