In aircraft design, the “radius of a turboshaft” typically refers to the distance from the center of the engine’s hub to the outer edge or tip of the turbine section of the engine. Turboshaft engines are a type of gas turbine engine used in helicopters and certain aircraft to provide mechanical power to drive components such as the main rotor.
Formula for Radius of Turboshaft Engine (r):The formula to calculate the radius of a turboshaft engine depends on the specific design and geometry of the engine. For a simple circular engine, you can use the following formula:
Radius (r) is typically measured in meters (m).