Fundamentals of Heat Engines. Jamil Ghojel

Fundamentals of Heat Engines - Jamil Ghojel


Скачать книгу
is positive work.

Schema for a sign convention for heat and work.

      1.3.5 First Law of Thermodynamics

equation

      Considered here are applications of the first law in two engineering energy systems: non‐flow system and steady‐flow system.

      1.3.5.1 Non‐Flow Energy Equation

      For a closed system (no flow of fluid) that does not execute a cycle, the energy equation is

      where

      ∑Q: total heat transfer

      ∑W: total work transfer

      ΔU: internal energy change

      The sign convention for work and heat is shown in Figure 1.9

      1.3.5.2 Steady‐Flow Energy Equation

      1 Flow work or pressure work, given by pv.

      2 Kinetic energy C2/2, due to the movement of the fluid element with velocity C.

      3 Internal (thermal) energy u, due to the energy of the fluid molecules.

      4 Potential or gravimetric energy, due to the height z above some datum line and given by zg.

      5 Chemical, electrical, or magnetic energies may also be added, but these are not involved in the overwhelming cases encountered in thermal power cycles.

      6 Heat Q may enter or leave the control volume.

      7 Mechanical energy W may be added or removed, with some of the added energy being used to pump the fluid into the control volume or expel it out again.

      8 Accumulated (stored) energy in the control volume as a whole ecv.

Schema for steady-state, steady-flow control volume. equation

      Energy is not usually allowed to accumulate in the control volume of practical thermal power plants operating on thermodynamic cycles, and therefore the term ecv will be henceforward ignored and the energy equation is reduced to

      Since specific enthalpy h = u + pv, Eq. (1.59) can be rewritten as

      For a fluid flowing steadily at the rate of images kg/s, the energy equation becomes

      where

equation

      All terms in Eq. (1.61) have units of power (images).

      For a control volume with multiple flows into and out of the system, the general steady‐flow energy equation can be written as

      1.3.5.3 Stagnation Properties

      The stagnation enthalpy ht is the enthalpy that a gas stream of enthalpy h and velocity C would possess when brought to rest adiabatically and without work transfer. The energy equation thus becomes

equation

      (1.63)equation

      For a perfect gas, h = cpT and the corresponding stagnation temperature Tt is

      Applying the concept of stagnation properties to an adiabatic compression, the energy Eq. (1.60) becomes

equation

      Rearranging, we get

      (1.65)equation

      Temperature‐measuring devices such as thermometers and thermocouples in reality measure the stagnation temperature of the flow and not the static temperature. Thus, introduction of stagnation temperatures simplifies solving the energy equation by eliminating the kinetic energy term and the need to measure flow velocity.

      The stagnation pressure pt is defined as the pressure the gas stream would possess if the gas were brought to rest adiabatically and reversibly. Using Eqs. (1.48) and Скачать книгу