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Gas Power Cycle In Engineering Thermodynamics by PK NAG (Chapter-13) banner
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Gas Power Cycle In Engineering Thermodynamics by PK NAG (Chapter-13)

Gas Power Cycle In Engineering Thermodynamics by PK NAG (Chapter-13) banner
Preview this course
Self-paced Beginner

Gas Power Cycle In Engineering Thermodynamics by PK NAG (Chapter-13)

4(144)
14 enrolled
2654 views
₹ 499
318 min
Anytime
Hindi
2654 views
Saurabh Kumar Gupta
Saurabh Kumar GuptaMechanical Engineer
  • 7-day money-back guarantee
  • Lifetime access
  • Certificate of completion
Volume pricing for groups of 5+

Why enroll

This course is based on PK Nag's Book Chapter 13, to excel in the GATE (Graduate Aptitude Test in Engineering) examination and to secure good marks in other engineering exams. Thermodynamics is a crucial subject in the engineering syllabus, and mastering the concepts and applications presented in Chapter 13 is essential to achieving a high score. By taking this course, individuals can gain a comprehensive understanding of thermodynamic principles, practice solving problems, and develop strategies to tackle complex questions. With a strong foundation in thermodynamics, students can confidently approach the GATE exam and improve their chances of securing admission to top engineering programs or landing coveted jobs at top PSUs.

Master the fundamentals of thermodynamics and unlock the secrets of energy conversion, efficiency, and optimization—enroll now and become a thermal energy expert!

What enrolled engineers say

6 verified reviews
  • May 3, 2026

    Chapter 13's Brayton cycle walkthrough, especially the regeneration + intercooling T–s plot example, made the efficiency math stick; the step where pressure ratio shifts optimum was an obs. Mostly clear, though wasn't sold on the quick jump to aerospace turbines, and I wished there was one more worked problem tying numbers to hvacr-scale gas turbines.

    aloķ Y. Verified
  • May 3, 2026

    Chapter 13’s Brayton cycle worked example with regenerator effectiveness—walking T2/T4 on the T‑s plot—made efficiency vs pressure ratio click fast. As a bootcamp grad, it maps cleanly to gas turbines in prod arch, but I wasn't sold on the skim of intercooling; wished for one more numeric pass.

    Devavrath R. Verified
  • May 3, 2026

    This is the kind of material you reach for when the arch starts wobbling and you need first principles, not another layer of tooling. Chapter 13’s walk-through of the Brayton cycle with regeneration, especially the bit where effectiveness shifts thermal efficiency step by step, stuck with me; it reads like tracing a legacy repo before opening a PR. The equations weren’t abstracted away, but they also weren’t dumped, which helped bridge textbook gas turbines to how we reason about constraints in prod infra. Coming from modern stacks (k8s, CI, watching RPS graphs), the T–s diagrams felt like an older obs view, but they map cleanly once you sit with them. It’s beginner-friendly mostly, though I wasn’t sold on how briefly intercooling vs reheating tradeoffs were treated; one more numeric example would’ve helped. Still, it gives a clear path from basics to confidence, the kind that supports growth when you have to rebuild understanding from the ground up.

    Nitin K. · student Verified

Is this course for you?

You should take this if

  • You work in Aerospace or HVAC
  • You're a Chemical & Process / Mechanical Engineering professional
  • You prefer self-paced learning you can revisit

You should skip if

  • You need a different specialisation outside Chemical & Process
  • You need live interaction with an instructor

Course details

A gas power cycle, commonly known as the Brayton cycle, is a thermodynamic cycle used in gas turbine engines to generate power. In this cycle, air is first drawn from the atmosphere and compressed in a compressor, which increases its pressure and temperature. The compressed air then enters a combustion chamber, where fuel is added and burned at nearly constant pressure, resulting in a significant rise in temperature. This high-temperature, high-pressure gas expands through a turbine, producing useful work; part of this work is used to drive the compressor, while the remaining can be used for power generation. Finally, the exhaust gases are released to the atmosphere at approximately constant pressure, completing the cycle.

The efficiency of a gas power cycle depends mainly on the pressure ratio and the maximum temperature achieved during combustion, and it can be improved through methods such as regeneration, intercooling, and reheating.

Course suitable for

Key topics covered

  • Introduction to Gas Power Cycle

  • Otto Cycle

  • Diesel Cycle

  • Dual Cycle

  • Comparison of Otto, Diesel or Dual

  • Numerical on Otto Cycle

  • Numerical on Diesel Cycle

  • Numerical on Dual Cycle

  • Brayton Cycle

  • Actual Brayton Cycle Analysis

  • Effect of Pressure Ratio

  • Regeneration on Brayton Cycle

  • Reheating on Brayton Cycle

Course content

The course is readily available, allowing learners to start and complete it at their own pace.

12 lectures5 hr 18 min
  1. Introduction to Gas Power Cycle | Mean Effective Pressure
    24 min
  2. Otto Cycle | Mean Effective pressure of otto cycle
    36 min
  3. Diesel Cycle || Mean Effective Pressure of Diesel cycle
    38 min
  4. Dual Cycle || Limited Pressure cycle || Mean Effective Pressure
    32 min
  5. Comparison of Otto cycle, dual cycle and diesel cycle
    14 min
  6. Numerical on Pk Nag Book Based on Otto Cycle
    18 min
  7. Numerical on Diesel Cycle
    10 min
  8. Numerical on Dual Cycle Pk Nag Book
    24 min
  9. Ideal Brayton Cycle || Gas Turbines || Gas Power Cycle
    42 min
  10. Actual Brayton Cycle Analysis | Work ratio || Gas Turbines
    24 min
  11. Effect of pressure ratio on Brayton cycle | Optimum pressure
    28 min
  12. Regeneration on Brayton Cycle || Gas Turbines
    28 min

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Questions and Answers

A: Governing principle: Net work in an ideal Brayton cycle scales with cp·(T3−T4−(T2−T1)). With r_p≈6, T3=1200 K, and air-standard relations, T4 drops to ~700 K and T2 rises to ~500 K, leaving a few hundred kJ/kg. That order survives first-pass losses. Option B traps engineers who remember that low pressure ratios cancel out, but import that intuition beyond its range here.

A: Governing principle: Thermal efficiency follows the balance between added turbine work and added compressor work. At fixed T3 there’s a clear optimum r_p; below it, gains dominate, above it, compression penalty wins. Option B snares people who extrapolate low‑r_p textbook plots without checking the fixed‑T3 constraint.

A: Governing principle: For a given pressure ratio, lower compressor efficiency increases temperature rise. Fouling fits the symptom and the time-in-service trend, and it feeds directly into higher thermal stress assumptions. Option C catches engineers who know inlet temperature matters but miss that the delta observed exceeds ambient variation.

A: Governing principle: Back work ratio is W_c/W_t, not net over gross. For air-standard Brayton cycles with moderate r_p, compressor work is a large fraction but not all of turbine work. Option C tempts those who confuse shaft power balance with thermodynamic work terms.