To solve this problem, we must understand the behavior of Rayleigh flow, which is the flow of a compressible fluid in a constant area duct where heat is added or removed without friction. In Rayleigh flow, the following key points should be noted:
- Total Temperature (Tt): The total temperature, or stagnation temperature, increases when heat is added. This is due to the conservation of energy principle, where the added heat increases the energy of the system, thus increasing the total temperature for both supersonic and subsonic flows.
- Total Pressure (Pt): The total pressure decreases due to the irreversible nature of heat addition. Despite being a frictionless process, entropy increases, leading to a loss in total pressure for both supersonic and subsonic flows.
Given the above principles, the statement that "Total temperature increases and total pressure decreases for both supersonic and subsonic flows at inlet" accurately describes the behavior of Rayleigh flow.