The length of the combustion chamber in a “can-type” combustion chamber for aircraft design refers to the axial length or height of the combustion chamber. This parameter is essential for understanding the chamber’s size and geometry, which affects combustion efficiency and engine performance.
The formula to calculate the length of the combustion chamber is as follows:
- Length of Combustion Chamber is the axial length or height of the combustion chamber, typically measured in meters (m) or feet (ft).
- Volume is the internal volume of the combustion chamber, typically measured in cubic meters (m³) or cubic feet (ft³).
- Diameter of Combustion Chamber is the internal diameter of the combustion chamber, typically measured in meters (m) or feet (ft).
- π (pi) is a mathematical constant approximately equal to 3.14159.