In aircraft design, the “radius of a turboprop” typically refers to the distance from the center of the engine’s hub to the outer edge or tip of the propeller blades in the engine’s propeller section. Turboprop engines are a type of aircraft propulsion system that combines a gas turbine engine with a propeller for generating thrust.
Formula for Radius of Turboprop Engine (r):The formula to calculate the radius of a turboprop engine depends on the specific design and geometry of the engine. For a simple circular propeller, you can use the following formula:
- Radius (r) is typically measured in meters (m).