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GATE Marine Engineering Thermodynamics and Marine Engineering Syllabus

The Thermodynamics and Marine Engineering syllabus for GATE Marine Engineering in full: 6 chapters, 16 topics and 98 sub-topics, every one listed below, plus 50 Thermodynamics and Marine Engineering flashcards with answers.

6Chapters
16Topics
98Sub-topics
50Flashcards

Thermodynamics and Marine Engineering syllabus: all 6 chapters

Expand any chapter to see its topics and sub-topics.

  1. Thermodynamics

    4 topics
    • First law of thermodynamics
      • Closed system undergoing a cycle
      • Closed system undergoing a change of state
      • Internal energy of a system
      • Expansion work
      • Process using ideal gas - constant pressure, constant volume, isothermal
      • Adiabatic and polytropic process - work done and heat added in different process
      • First law applied to one-dimensional steady flow process
      • Flow energy
      • Steady flow energy equation (ID)
    • Second law of Thermodynamics
      • Different statements
      • Reversible and irreversible process
      • Corollaries of the second law
      • Absolute temperature scale
      • Carnot cycle - Carnot engine, refrigerator, and heat pump
      • Clausius inequality and definition of entropy
      • Change of entropy of an ideal gas
    • Gas power cycles and I.C. Engines
      • Gas power cycles: Carnot cycle, Brayton cycle, Erricson cycle, Sterling cycle etc.
      • Air standard cycles: Otto-Diesel, Dual, and Joule cycle
      • Evaluation of thermal efficiency and mean effective pressure
      • Internal Combustion engine - Classification of I.C. engines
      • Principle of operation of spark Ignition and Compression Ignition engines
      • Stages of combustion in S.I. and C.I. engines
      • Knocking and detonation - factors controlling knock and detonation
      • Methods of preventing Knocking and detonation
    • Refrigeration
      • Principle of operation of Simple vapour compression system
      • Comparison with vapour compression systems
      • Air conditioning principles
      • Sensible heating and cooling
      • Humidification and dehumidification
      • Cooling and humidification
      • Cooling and dehumidification
      • Heating and humidification
      • Heating and dehumidification
      • Adiabatic mixing of air streams - cooling and heating load calculation
  2. Marine Diesel Engines

    1 topic
    • General engine principles
      • Low speed and medium speed diesel engines
      • Two and Four-stroke engines
      • Scavenging and turbocharging
      • Fuel oil system
      • Lubricating oil systems
      • Cooling systems
      • Torque and power measurement
      • Starting air systems and reversing systems
      • Controls and safety devices
      • Couplings and Gearboxes
      • Specific Fuel Consumption
      • Waste heat recovery system
      • MARPOL regulations and Energy Efficiency Design Index (EEDI)
      • Ship Energy Efficiency Management Plan (SEEMP)
  3. Marine Steam Turbines

    4 topics
    • Types of turbines
      • Compounding
      • Reheat
      • Turbine construction
      • Rotors
      • Blades
      • Casing
      • Gland sealing
      • Diaphragms
      • Nozzles
      • Bearings
    • Lubrication systems
      • Expansion arrangements
      • Gearings
    • Marine gas turbines
      • Fundamentals of G.T.
      • Structure of gas turbines
      • Gearing
      • Operational features
      • Controls
      • Combined cycles
    • Nuclear propulsion
      • Physical principles of the operation of nuclear reactors
      • Use of nuclear propulsion on seagoing vessels
      • Electrical Propulsion
  4. Marine Boilers

    2 topics
    • Types of boilers
      • Fire tube
      • Water tube boilers
      • Package boilers
      • Cochran Boilers
      • Composite boilers
      • Steam to steam generators
      • Double evaporation boilers
      • Exhaust gas heat exchangers
      • Auxiliary steam plant systems
      • Exhaust gas boilers
      • Composite boilers
    • Boiler mounting
      • Combustion
      • Feed system
      • Feed water treatment
  5. Engine Dynamics

    1 topic
    • Torsional vibration of engine and shafting
      • Axial shaft vibration
      • Critical speeds
      • Engine rating
      • Rating corrections
      • Trial tests
  6. Marine Auxiliary Machinery & Systems

    4 topics
    • Different types of pumps and piping systems in ships
      • Hot water, drinking water, cooling water, and seawater systems
      • Fuel oil systems
      • Lubricating oil system filters, coolers, centrifuges, purifiers, and clarifiers
      • Bilge and ballast systems
      • Sewage disposal systems
      • Oily water separator
      • Air compressors
      • Boilers
      • Heat exchangers
      • Waste heat recovery systems
    • Heat, ventilation and air conditioning systems
    • Deck machinery and cargo handling systems
    • Propulsions and steering gear systems

GATE Marine Engineering Thermodynamics and Marine Engineering flashcards — 50 questions with answers

  1. State the First Law of Thermodynamics for a closed system undergoing a process.

    For a closed system, the heat added equals the change in internal energy plus the work done: $$Q = \Delta U + W$$ Equivalently, in differential form, $\delta Q = dU + \delta W$. It expresses conservation of energy.

  2. What does the First Law state for a closed system undergoing a complete cycle?

    The cyclic integral of heat equals the cyclic integral of work: $$\oint \delta Q = \oint \delta W$$ Since the system returns to its initial state, $\oint dU = 0$, so net heat transfer equals net work over the cycle.

  3. Why does internal energy $U$ qualify as a property (point function) of a system?

    Because its cyclic integral is zero, $\oint dU = 0$. Its change between two states depends only on the end states and not on the path, so $dU$ is an exact differential and $U$ is a point function (property).

  4. Distinguish a point function from a path function, giving an example of each.

    A point function depends only on the state (e.g., internal energy $U$, pressure, temperature) and has an exact differential. A path function depends on the process path (e.g., work $W$ and heat $Q$) and has an inexact differential ($\delta W$, $\delta Q$).

  5. What is internal energy of a system, and on what does it depend for an ideal gas?

    Internal energy is the total energy stored within the system due to molecular motion and configuration. For an ideal gas it is a function of temperature only: $U = U(T)$, and $dU = m c_v \, dT$.

  6. Write the expression for expansion (displacement) work done by a closed system during a quasi-static process.

    $$W = \int_{1}^{2} p \, dV$$ This represents the area under the process curve on a $p\text{-}V$ diagram for a reversible (quasi-static) process.

  7. Give the work done by an ideal gas in a constant-pressure (isobaric) process.

    $$W = \int_{1}^{2} p \, dV = p(V_2 - V_1) = mR(T_2 - T_1)$$

  8. What is the work done in a constant-volume (isochoric) process, and where does the heat go?

    Since $dV = 0$, the work is $W = \int p\, dV = 0$. By the First Law, all heat added raises internal energy: $Q = \Delta U = m c_v (T_2 - T_1)$.

  9. Derive the work done by an ideal gas during a reversible isothermal process.

    With $pV = $ constant, $$W = \int_{1}^{2} p\, dV = p_1 V_1 \ln\frac{V_2}{V_1} = mRT \ln\frac{V_2}{V_1} = mRT \ln\frac{p_1}{p_2}$$

  10. For a reversible isothermal process of an ideal gas, what is the heat transfer?

    Since $\Delta U = 0$ (temperature constant, $U=U(T)$), the First Law gives $Q = W = mRT \ln\dfrac{V_2}{V_1}$. All heat added is converted to work.

  11. Define an adiabatic process and write its governing $p\text{-}V$ relation for an ideal gas.

    An adiabatic process has no heat transfer, $Q = 0$ (system thermally insulated). For a reversible adiabatic process of an ideal gas: $$pV^{\gamma} = \text{constant}, \quad \gamma = \frac{c_p}{c_v}$$

  12. Give the work done by an ideal gas during a reversible adiabatic process.

    $$W = \frac{p_1 V_1 - p_2 V_2}{\gamma - 1} = \frac{mR(T_1 - T_2)}{\gamma - 1}$$ Since $Q=0$, this work equals the decrease in internal energy: $W = -\Delta U = m c_v (T_1 - T_2)$.

  13. Write the temperature-volume and temperature-pressure relations for a reversible adiabatic process.

    $$\frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{\gamma - 1} = \left(\frac{p_2}{p_1}\right)^{\frac{\gamma - 1}{\gamma}}$$

  14. Define a polytropic process and state its $p\text{-}V$ relation.

    A polytropic process follows $$pV^{n} = \text{constant}$$ where $n$ is the polytropic index. Special cases: $n=0$ (isobaric), $n=1$ (isothermal), $n=\gamma$ (adiabatic), $n=\infty$ (isochoric).

  15. What is the work done during a reversible polytropic process ($pV^n = C$)?

    $$W = \frac{p_1 V_1 - p_2 V_2}{n - 1} = \frac{mR(T_1 - T_2)}{n - 1}$$

  16. Give the heat transferred during a polytropic process of an ideal gas.

    $$Q = \left(\frac{\gamma - n}{\gamma - 1}\right) W = m c_n (T_2 - T_1)$$ where the polytropic specific heat is $c_n = c_v \dfrac{\gamma - n}{1 - n}$.

  17. What are the polytropic temperature relations in terms of volume and pressure ratios?

    $$\frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{n-1} = \left(\frac{p_2}{p_1}\right)^{\frac{n-1}{n}}$$

  18. What is flow energy (flow work), and what is its expression per unit mass?

    Flow energy is the work required to push fluid across a boundary by the pressure of surrounding fluid. Per unit mass it equals $pv$ (pressure times specific volume), i.e. $p/\rho$. It is associated with mass entering or leaving an open system.

  19. Write the general Steady Flow Energy Equation (SFEE) per unit mass for a one-inlet, one-outlet device.

    $$h_1 + \frac{V_1^{2}}{2} + g z_1 + q = h_2 + \frac{V_2^{2}}{2} + g z_2 + w$$ where $h$ is specific enthalpy, $V$ velocity, $z$ elevation, $q$ heat and $w$ work per unit mass.

  20. What two key assumptions define a steady-flow process?

    (1) The mass flow rate and all properties at each point are constant in time (nothing accumulates); $\dfrac{dm_{cv}}{dt}=0$ and $\dfrac{dE_{cv}}{dt}=0$. (2) The state of the fluid at any given location does not change with time.

Show the other 30 Thermodynamics and Marine Engineering flashcards
  1. Why does enthalpy $h = u + pv$ appear naturally in the SFEE?

    In a flow process each fluid stream carries both its internal energy $u$ and flow work $pv$. Their sum, $u + pv = h$, combines automatically, so enthalpy represents the total energy transported by the flowing fluid per unit mass.

  2. Apply the SFEE to a nozzle (adiabatic, no work, negligible $\Delta z$). What is the result?

    With $q=0$, $w=0$, $\Delta z \approx 0$: $$h_1 + \frac{V_1^{2}}{2} = h_2 + \frac{V_2^{2}}{2}$$ so $V_2 = \sqrt{2(h_1 - h_2) + V_1^{2}}$. Enthalpy drop is converted to kinetic energy.

  3. Apply the SFEE to an adiabatic turbine (negligible KE and PE changes).

    With $q=0$ and $\Delta KE \approx \Delta PE \approx 0$: $$w = h_1 - h_2$$ The work output per unit mass equals the enthalpy drop across the turbine.

  4. What does the SFEE reduce to for a throttling (porous plug/valve) process?

    For throttling: $q=0$, $w=0$, negligible $\Delta KE$ and $\Delta PE$, giving $$h_1 = h_2$$ Throttling is an isenthalpic process (constant enthalpy).

  5. State the Kelvin-Planck statement of the Second Law of Thermodynamics.

    It is impossible to construct a device operating in a cycle that produces no effect other than the extraction of heat from a single reservoir and the production of an equivalent amount of work. No engine can have 100% thermal efficiency.

  6. State the Clausius statement of the Second Law of Thermodynamics.

    It is impossible to construct a device operating in a cycle whose sole effect is the transfer of heat from a cooler body to a hotter body. Heat cannot flow spontaneously from low to high temperature without external work.

  7. Are the Kelvin-Planck and Clausius statements equivalent?

    Yes. They are two equivalent expressions of the Second Law: a violation of one implies a violation of the other. This is proved by showing that a hypothetical device violating one statement could be coupled to produce a violation of the other.

  8. Define a reversible process and list conditions for reversibility.

    A reversible process can be reversed so that both the system and surroundings return to their initial states with no net change. Conditions: quasi-static (infinitesimally slow), no friction, no unrestrained expansion, no heat transfer across a finite temperature difference, no mixing/dissipative effects.

  9. Define an irreversible process and give common causes of irreversibility.

    An irreversible process cannot be reversed without leaving permanent changes in the surroundings. Causes include friction, unrestrained (free) expansion, heat transfer through a finite temperature difference, mixing, throttling, inelastic deformation, and chemical reactions.

  10. State the Carnot Theorem (a corollary of the Second Law).

    No heat engine operating between two given thermal reservoirs can be more efficient than a reversible (Carnot) engine operating between the same two reservoirs. Hence $\eta_{irrev} < \eta_{rev}$.

  11. State the corollary of Carnot's theorem regarding all reversible engines.

    All reversible engines operating between the same two thermal reservoirs have the same efficiency, independent of the working substance. Their efficiency depends only on the reservoir temperatures.

  12. How is the thermodynamic (absolute) temperature scale defined using a reversible engine?

    For a reversible engine the ratio of heat transfers equals the ratio of absolute temperatures: $$\frac{Q_1}{Q_2} = \frac{T_1}{T_2}$$ This defines the Kelvin (absolute) temperature scale, independent of any thermometric substance.

  13. List the four reversible processes that make up the Carnot cycle.

    (1) Reversible isothermal heat addition at $T_H$, (2) reversible adiabatic (isentropic) expansion, (3) reversible isothermal heat rejection at $T_L$, and (4) reversible adiabatic (isentropic) compression back to the start.

  14. Write the thermal efficiency of a Carnot heat engine.

    $$\eta_{Carnot} = 1 - \frac{Q_L}{Q_H} = 1 - \frac{T_L}{T_H}$$ where temperatures are absolute (Kelvin). It is the maximum possible efficiency between reservoirs at $T_H$ and $T_L$.

  15. Write the coefficient of performance (COP) of a Carnot refrigerator.

    $$\text{COP}_{ref} = \frac{Q_L}{W_{net}} = \frac{Q_L}{Q_H - Q_L} = \frac{T_L}{T_H - T_L}$$ where $Q_L$ is heat removed from the cold space.

  16. Write the coefficient of performance (COP) of a Carnot heat pump.

    $$\text{COP}_{hp} = \frac{Q_H}{W_{net}} = \frac{Q_H}{Q_H - Q_L} = \frac{T_H}{T_H - T_L}$$ Also, $\text{COP}_{hp} = \text{COP}_{ref} + 1$.

  17. State the Clausius Inequality.

    For any cyclic process, $$\oint \frac{\delta Q}{T} \leq 0$$ Equality holds for a reversible cycle; the inequality ($<0$) holds for an irreversible cycle. $T$ is the absolute temperature of the boundary where $\delta Q$ crosses.

  18. How is entropy defined from the Clausius inequality?

    Since $\oint (\delta Q/T)_{rev} = 0$, the quantity $(\delta Q/T)_{rev}$ is an exact differential of a property called entropy: $$dS = \left(\frac{\delta Q}{T}\right)_{rev}$$ Entropy is a point function with units $\mathrm{J/K}$.

  19. What is the relation between entropy change and heat for reversible vs irreversible processes?

    $$dS \geq \frac{\delta Q}{T}$$ Equality ($dS = \delta Q/T$) for a reversible process; inequality ($dS > \delta Q/T$) for an irreversible process. The difference is entropy generated by irreversibility.

  20. State the principle of increase of entropy for an isolated system.

    For an isolated system (no heat or work crossing the boundary) entropy can never decrease: $$dS_{iso} \geq 0$$ It increases for irreversible processes and stays constant for reversible ones, defining the direction of spontaneous change.

  21. Write the entropy change of an ideal gas in terms of temperature and volume.

    $$\Delta S = m\left( c_v \ln\frac{T_2}{T_1} + R \ln\frac{V_2}{V_1} \right)$$

  22. Write the entropy change of an ideal gas in terms of temperature and pressure.

    $$\Delta S = m\left( c_p \ln\frac{T_2}{T_1} - R \ln\frac{p_2}{p_1} \right)$$

  23. Write the entropy change of an ideal gas in terms of pressure and volume.

    $$\Delta S = m\left( c_v \ln\frac{p_2}{p_1} + c_p \ln\frac{V_2}{V_1} \right)$$

  24. What is the entropy change of an ideal gas during a reversible isothermal process?

    With $T_2 = T_1$: $$\Delta S = mR \ln\frac{V_2}{V_1} = mR \ln\frac{p_1}{p_2} = \frac{Q}{T}$$

  25. What is the entropy change in a reversible adiabatic process, and what is such a process called?

    Since $\delta Q = 0$ and the process is reversible, $\Delta S = 0$. The process is isentropic (constant entropy).

  26. Write the two Tds (Gibbs) equations relating entropy to other properties.

    $$T\,dS = dU + p\,dV \quad\text{(first Tds equation)}$$ $$T\,dS = dH - V\,dp \quad\text{(second Tds equation)}$$ These hold for any simple compressible substance.

  27. Compare heat and work added in isothermal vs adiabatic expansion of an ideal gas between the same volume ratio.

    Isothermal: $T$ constant, $\Delta U=0$, all heat added becomes work, $Q=W=mRT\ln(V_2/V_1)$. Adiabatic: $Q=0$, work is done at the expense of internal energy so temperature falls, $W = -\Delta U = mc_v(T_1-T_2)$. For the same volume ratio, isothermal work exceeds adiabatic work.

  28. Relate the polytropic index $n$ to whether heat is added or rejected during gas expansion (with $1<n<\gamma$).

    For expansion with $1<n<\gamma$, the factor $\dfrac{\gamma-n}{\gamma-1}>0$, so $Q$ and $W$ have the same sign: heat is added to the gas while it does positive work. The specific heat $c_n = c_v\dfrac{\gamma-n}{1-n}$ is negative in this range.

  29. What is a perpetual motion machine of the second kind (PMM2)?

    A PMM2 is a hypothetical device that produces work continuously while exchanging heat with only a single reservoir, i.e. with 100% efficiency. It violates the Kelvin-Planck statement of the Second Law and is impossible to build.

  30. Define a thermal reservoir and distinguish a source from a sink.

    A thermal reservoir is a body with very large heat capacity that can supply or absorb finite heat without any change in its temperature. A source supplies heat (e.g., furnace at $T_H$); a sink absorbs heat (e.g., atmosphere at $T_L$).

GATE Marine Engineering Thermodynamics and Marine Engineering FAQ

What is in the GATE Marine Engineering Thermodynamics and Marine Engineering syllabus?

GATE Marine Engineering Thermodynamics and Marine Engineering is split into 6 chapters: Thermodynamics, Marine Diesel Engines, Marine Steam Turbines, Marine Boilers, Engine Dynamics and Marine Auxiliary Machinery & Systems. Together they contain 16 topics and 98 sub-topics.

How many chapters are in GATE Marine Engineering Thermodynamics and Marine Engineering?

6 chapters, containing 16 topics and 98 sub-topics. The largest chapter is Thermodynamics, with 4 topics.

Are there flashcards for GATE Marine Engineering Thermodynamics and Marine Engineering?

Yes — a 50-card Thermodynamics and Marine Engineering deck, printed in full in the flashcards section of this page and available in the Examius app with spaced repetition. The free plan covers one exam of your choice, including its flashcards; Examius Pro, a one-time purchase, unlocks every other exam and deck.