The mass of each internal component in a can-annular combustion chamber in aircraft design refers to the individual mass of the specific components or parts located inside the combustion chamber, which are necessary for the combustion process. These internal components can include items such as burners, igniters, fuel injectors, liners, and other elements that play a role in the combustion of air and fuel.
The formula to calculate the mass of each internal component is straightforward and may vary depending on the specific component being considered. In general, it can be expressed as:
- Mass of Each Internal Component is the individual mass of the specific internal component, typically measured in kilograms (kg) or pounds (lb).
- Volume of the Component is the volume occupied by that particular component within the combustion chamber, typically measured in cubic meters (m³) or cubic feet (ft³).
- Material Density is the density of the material from which the component is constructed, typically measured in kilograms per cubic meter (kg/m³) or pounds per cubic foot (lb/ft³).