TITLE.PM5

(xx) ENGINEERING THERMODYNAMICS dharm \M-therm\th0-1 Power : 1 watt = 1 joule/sec = 0.860 kcal/h 1 h.p. = 75 m kgf/sec = 0.1757 ...

INTRODUCTION TO SI UNITS AND CONVERSION FACTORS (xxi) dharm \M-therm\th0-1 Nomenclature A area b steady-flow availability functi ...

(xxii) ENGINEERING THERMODYNAMICS dharm \M-therm\th0-1 Q heat, rate of heat transfer q rate of heat transfer per unit area R gas ...

1 1.1. STEAM POWER PLANT 1.1.1. Layout Refer to Fig. 1.1. The layout of a modern steam power plant comprises of the following fo ...

2 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 Econo- miser Flue gases Steam turbine Generator Cooling tower Pump Feed wa ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 3 dharm \M-therm\Th1-1.pm5 Condenser. It condenses steam used by the steam tur ...

4 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 1.3. Internal Combustion Engines 1.3.1. Heat engines Any type of engine or ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 5 dharm \M-therm\Th1-1.pm5 Exhaust valve Rocker arm Petrol tank Engine throttle ...

6 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 I.V. E.V. Air-fuel mixture S.P. I.V. E.V. S.P. S.P. S.P. E.C. C.R. C Exhau ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 7 dharm \M-therm\Th1-1.pm5 the charge gets compressed when E.P. (exhaust port) ...

8 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 turbine represents perhaps the most satisfactory way of producing very lar ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 9 dharm \M-therm\Th1-1.pm5 The components of the gas turbine can be made light ...

10 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 and the rest is utilised in electrical energy. The gas turbines work on o ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 11 dharm \M-therm\Th1-1.pm5 The flow diagram of such a cycle is shown in Fig. 1 ...

12 ENGINEERING THERMODYNAMICS dharm \M-therm\Th1-1.pm5 Condenser (wire-tube type) High pressure gas Compre- Discharge line ssor ...

INTRODUCTION—OUTLINE OF SOME DESCRIPTIVE SYSTEMS 13 dharm \M-therm\Th1-1.pm5 — Combustor — Auxiliaries such as starting device, ...

2 Basic Concepts of Thermodynamics 2.1. Introduction to kinetic theory of gases. 2.2. Definition of thermodynamics. 2.3. Thermod ...

BASIC CONCEPTS OF THERMODYNAMICS 15 dharm M-therm/th2-1.pm5 Pressure exerted by an Ideal Gas : Let us consider a quantity of gas ...

16 ENGINEERING THERMODYNAMICS dharm M-therm/th2-1.pm5 According to Newton’s second law of motion the rate of change of ‘momentum ...

BASIC CONCEPTS OF THERMODYNAMICS 17 dharm M-therm/th2-1.pm5 or pV= m NC 1 3 (^2) ...(2.2) This equation is the fundamental equat ...