The first law for open systems (control volumes) extends closed-system analysis by accounting for mass flow across boundaries, leading to the steady-flow energy equation. Each unit of mass carries enthalpy h with it into and out of the device, in addition to kinetic and potential energy. This framework enables analysis of pumps, turbines, compressors, and piping systems where fluid moves continuously through a device.
Derive the steady-flow energy equation from first principles by tracking mass and energy entering and leaving a control volume. Practice with devices where kinetic energy effects are small (turbines, compressors, heat exchangers) before tackling high-velocity flow. Recognize that enthalpy h = u + Pv naturally appears because flowing fluid must do flow work Pv to enter and exit the device.
The first law for closed systems — ΔU = Q − W — tracks energy for a fixed mass of substance with no material crossing the boundary. Most real engineering devices (turbines, pumps, compressors, boilers) operate differently: fluid flows continuously in and out while the device itself reaches a steady operating state. Analyzing these requires extending the first law to open systems, or control volumes, where mass crosses the boundary.
The crucial difference from closed systems is that flowing mass carries energy with it. A parcel of fluid entering a device has internal energy u per unit mass, but it also does work pushing the fluid column behind it into the device — this is called flow work, and its magnitude is Pv per unit mass (pressure times specific volume). The total energy that each unit of mass transports across the boundary is therefore u + Pv, which is the definition of specific enthalpy h. This is not a coincidence or a definition of convenience; it is a direct consequence of writing the first law for a control volume with moving boundaries. Enthalpy h naturally replaces internal energy u in open-system analysis for exactly this reason.
For a single-inlet, single-outlet device at steady state, the energy equation becomes Q̇ − Ẇ_s = ṁ[(h₂ − h₁) + ½(V₂² − V₁²) + g(z₂ − z₁)], where Q̇ is the rate of heat transfer, Ẇ_s is shaft work (turbine output or pump input), and ṁ is the mass flow rate. The terms involving kinetic and potential energy can often be dropped for devices like turbines and compressors, where enthalpy changes dominate. But for nozzles and diffusers — designed specifically to exchange enthalpy for kinetic energy — those terms are the entire purpose and cannot be neglected.
The steady-state assumption (dE_cv/dt = 0) is what makes this equation algebraic rather than differential: the energy inventory inside the device does not change over time, so every joule flowing in must flow out in some form. In practice, "steady" means the device has reached its operating condition — temperature and pressure at each point are stable, and mass flow rate is constant. Startup transients, where the device heats up or pressurizes, require the full unsteady form of the control-volume energy equation. Most engineering analysis focuses on the steady-state operating point, making the steady-flow energy equation one of the most widely used tools in thermodynamic analysis.