Subject Details
Dept     : AERO
Sem      : 4
Regul    : 2023
Faculty : Dr A Arun Negemiya
phone  : 9994421128
E-mail  : arunnegemiya.a.aero@snsct.org
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Lecture Notes

UNIT 1:
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Overview of propulsion systems and thermodynamic principles
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Types of aircraft engine
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Thrust equations and factors affecting thrust.
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Atomization and spray formation principles.
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Efficiency factors in aircraft propulsion
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Analysis of performance parameters of aircraft engines
UNIT 2:
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Introduction to ram effects and nozzle efficiency
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Analysis of shock swallowing by area variation
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Explore subsonic inlet stall and diffuser performance.
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Calculations on area ratios and thrust reversal scenarios
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Supersonic inlet starting problems and solutions.
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Real flow losses in nozzles.
UNIT 3:
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Introduction to gas turbine working principles and cycle.
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Simulations of turboprop, turbofan, and turbojet engines
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Thrust augmentation methods.
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Performance characteristics of turbine engines
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Comparative study of turboprop vs. turbojet engines.
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Efficiency and performance characteristics of gas turbines
UNIT 4:
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History and basic configurations of rockets.