The mass of structural components in a “can-type” combustion chamber refers to the total mass of the chamber’s structural elements, such as its walls, casing, and other load-bearing components that provide support and integrity to the chamber. This parameter is important for weight considerations and structural analysis in aircraft engine design.
The formula to calculate the mass of structural components is straightforward:
- Mass of Structural Components is the total mass of the combustion chamber’s structural elements, typically measured in kilograms (kg) or pounds (lb).
- Volume represents the total volume of the structural components, typically measured in cubic meters (m³) or cubic feet (ft³).
- Material Density is the density of the material used for the structural components, typically measured in kilograms per cubic meter (kg/m³) or pounds per cubic foot (lb/ft³).