Jamil Ghojel - Fundamentals of Heat Engines

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Summarizes the analysis and design of today’s gas heat engine cycles This book offers readers comprehensive coverage of heat engine cycles. From ideal (theoretical) cycles to practical cycles and real cycles, it gradually increases in degree of complexity so that newcomers can learn and advance at a logical pace, and so instructors can tailor their courses toward each class level. To facilitate the transition from one type of cycle to another, it offers readers additional material covering fundamental engineering science principles in mechanics, fluid mechanics, thermodynamics, and thermochemistry.
Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal-Combustion Engines Covers two main heat engines in one single reference Teaches heat engine fundamentals as well as advanced topics Includes comprehensive thermodynamic and thermochemistry data Offers customizable content to suit beginner or advanced undergraduate courses and entry-level postgraduate studies in automotive, mechanical, and aerospace degrees Provides representative problems at the end of most chapters, along with a detailed example of piston-engine design-point calculations Features case studies of design-point calculations of gas turbine engines in two chapters
can be adopted for mechanical, aerospace, and automotive engineering courses at different levels and will also benefit engineering professionals in those fields and beyond.

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Machine Working substance
Air compressor Air
Reciprocating and gas turbine engines Combustion products
Steam turbines Water vapour (steam)
Refrigerators Ammonia, CFCs, HCFCs

1.3.1 Work and Heat as Different Forms of Energy

Energy is the capacity a body or substance possesses that can result in the performance of mechanical work. The presence of energy can only be observed by its effects, which can appear in different forms such as work and heat. Other forms of energy include potential, kinetic, and internal. Energy cannot be created or destroyed, but it can be converted from one form to another. Mechanical work is the product of force and distance:

картинка 133

If F and S are at right angles to each other, no work can be done.

Heat is a manifestation of the degree of agitation of atoms and molecules making up a body as its temperature changes. It is also the effect of one system on another as a result of temperature inequality. Alternately, it can be said that heat is interaction that is not work.

картинка 134

A system is a region in space with boundaries across which matter, work, and heat can cross, as shown schematically in Figure 1.7. An example of a real system is a mass of gas or vapour contained in an engine cylinder, the boundary of which is comprised of the cylinder walls, cylinder head, and piston crown when the valves are closed.

Figure 17Schematic diagram of a thermodynamic system There are two types of - фото 135

Figure 1.7Schematic diagram of a thermodynamic system.

There are two types of systems:

Open system in which matter, heat, and work can pass through the system boundary

Closed system in which neither matter, heat, nor work pass through the system boundary

The state of the working fluid (matter) in a system is fully defined by two independent properties.

A property is a measurable characteristic of a system such as pressure, volume, temperature, energy, density, or a combination of the former such as internal energy, enthalpy, and entropy. Some measured properties were defined in Section 1.2, and temperature will be discussed in detail later, so we will define the derived (or combination) properties here.

Specific internal energy u is the intrinsic energy per unit mass of a fluid that is not in motion. Its value depends on its pressure and temperature unless the fluid is a perfect gas, in which case the specific internal energy will be dependent on temperature only. For a perfect gas, u = c v T

and for a mass m of the fluid,

Fundamentals of Heat Engines - изображение 136

Enthalpy is defined as H = U + pV kJ . Specific enthalpy is h = u + pv kJ / kg .

Entropy can be defined from the equation dQ = Tds , where T is the absolute thermodynamic temperature and s is the property entropy in units of J / mole . K .

A process is a change in a system from one state to another. Hence, the change in the pressure and temperature of a mass of gas from ( p 1, T 1) to ( p 2, T 2) is a process. The state defined by ( p 1, T 1) is the initial state of the system, and the state defined by ( p 2, T 2) is the final state of the system. Processes can be reversible or irreversible. In a reversible process, both the system and the surroundings are returned to their original conditions after the process and the reverse process had been carried out. In an irreversible process, reversal cannot be effected without leaving some change in the system or surroundings. Any process with friction (dry friction or viscous friction) is irreversible because some energy of the system is expended in overcoming friction and dissipated in the surroundings.

1.3.2 Mixture of Gases

For a mixture of N gaseous components, the total mass and total moles are, respectively,

where m i mass of the i th component n i amount of substance in moles of - фото 137 where m i mass of the i th component n i amount of substance in moles of - фото 138

where

m i: mass of the i th component

n i: amount of substance in moles of the i th component

If the molecular mass of i th component is μ i, then

(1.40) The mass fraction or mass concentration is 141 Similarly the mole - фото 139

The mass fraction (or mass concentration) is

(1.41) Similarly the mole fraction or mole concentration can be found as follows - фото 140

Similarly, the mole fraction (or mole concentration) can be found as follows:

(1.42) The molar mass of the total mixture is 143 - фото 141

The molar mass of the total mixture is

Fundamentals of Heat Engines - изображение 142

(1.43) Fundamentals of Heat Engines - изображение 143

From Eqs. (1.40), ( 1.41), and 1.42,

(1.44) Fundamentals of Heat Engines - изображение 144

Example 1.1

A gas mixture has the following mass composition:

Determine the molar composition of the mixture Solution - фото 145 Fundamentals of Heat Engines - изображение 146

Determine the molar composition of the mixture.

Solution

Fundamentals of Heat Engines - изображение 147
Gas % Mass fraction Mass fraction, c i Molecular mass, μ i Mole fraction, c i/ μ i % Mole fraction
CO 2 17.55 0.175 5 44 0.003 99 O 2 426 0042 6 32 0001 33 N 2 7633 0763 3 - фото 148
O 2 4.26 0.042 6 32 0.001 33 N 2 7633 0763 3 28 0027 26 CO 186 0018 6 2 - фото 149
N 2 76.33 0.763 3 28 0.027 26 CO 186 0018 6 28 0000 66 100 c i 10 - фото 150
CO 1.86 0.018 6 28 0.000 66 100 c i 10 c i μ i 003324 Total 100 1321 Dalton Model of Gas - фото 151
100 c i= 1.0 c i/ μ i= 0.03324 Total = 100

1.3.2.1 Dalton Model of Gas Mixtures

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