In aircraft design, the “Diameter of turbine blade” refers to the distance from the centerline of the turbine to the outer edge or tip of the blades in the turbine section of an aircraft engine. Turbine blades are responsible for extracting energy from the high-velocity exhaust gases to drive the engine’s compressor and other accessories.
Formula for Diameter of Turbine Blade (r):The formula to calculate the radius of a turbine blade depends on the specific design and geometry of the engine. For a simple circular turbine blade, you can use the following formula:
- Radius (r) is typically measured in meters (m).