In aircraft design, the “radius of compressor blade” typically refers to the distance from the center of the compressor to the outer edge or tip of the blades in the compressor section of an aircraft engine. The compressor blades are responsible for compressing incoming air before it enters the combustion chamber.
Formula for Radius of Compressor Blade (r):The formula to calculate the radius of a compressor blade depends on the specific design and geometry of the engine. For a simple circular compressor blade, you can use the following formula:
- Radius (r) is typically measured in meters (m).