Aerospace Propulsion

Introduction to Aerospace Propulsion

Aerospace Propulsion Aerospace Propulsion Aerospace Propulsion Digital World
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Introduction to Aerospace Propulsion
L1-Course Intro & Historical development of flights
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L2-Early development of aircraft propulsive devices
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L3-Development of Jet propulsion for aircraft
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L4- Introduction to thermodynamics, Scope and method, Basic concepts: system, surroundings, property, intensive and extensive, state, equilibrium and state postulate, process, path and cycle
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L5- Quasi-static processes, zeroth law of thermodynamics and temperature, concept of energy and its various forms, internal energy, enthalpy
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L6- Specific heats at constant pressure and volume Work and heat transfers
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L7- Tutorial
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L8- First law of thermodynamics for closed systems
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L9- First law of thermodynamics for open systems/flow processes
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L10-Second law of thermodynamics, heat engines, refrigerators and heat pumps, Kelvin-Planck and Clausius statement of second law of thermodynamics
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L11- Reversible and irreversible processes, concept of entropy
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L12- Increase of entropy principle, third law of thermodynamics, absolute entropy, perpetual motion machines
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L13- Tutorial
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L14- Carnot cycle, Carnot principle, thermodynamic temperature scale
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L15- Exergy, availability and second law efficiency
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L16- Tutorial
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L17- Gas and vapour power cycles, Otto cycle, Diesel cycle, Dual cycle
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L18- Rankine cycle, Brayton cycle, Stirling and Ericsson cycles
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L19- Thermodynamic property relations, Jacobean and Legendre transformations, Maxwell's equations
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L20- Tutorial
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Tutorial 2
L21- Properties of gas and vapour mixtures
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L22 (A)- One-dimensional compressible flows, isentropic flows
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L22 (B)- Flows with friction and heat transfer, normal and oblique shocks
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L23- Piston-prop engines: Otto cycles; Ideal and Real cycles
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L24- IC Engines for aircraft application
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L25- Performance parameters of IC engines
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L26- Supercharging of aircraft IC engines
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L27- Tutorial: IC Engines
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L28- Propeller fundamentals
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L29- Propeller aerodynamic theories -I
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L30- Propeller aerodynamic theories -II
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L31- Tutorial: Propellers
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L32- Ideal cycles for Jet engines
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L33- Ideal cycles for variants of jet engines
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L34- Tutorial
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L35- Fundamentals of Ramjets and Pulsejets
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L36- Fundamentals of Rocket engines
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L37- Fundamentals of Missile engines
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L38- Various space vehicles and their engines
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https://youtu.be/-0IdZanLwZs
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Exam
Introduction to Aerospace Propulsion
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About the course

Introduction to Propulsion :
The making of thrust to fly - science and history of propulsion; How the jet
engines make thrust : conceptual basis; Jet engine : Turbo-jet, Turbo-fans,
Turbo prop, Turbo-shaft.
Thermodynamic basis of Propulsion devices :
Basic concepts ; System-Boundary, Surroundings; State, Stable Equilibrium,
State Co-ordinates and parameters, Extensive and Intensive Parameters;
Energy interactions, Work and Heat transfers, Equilibrium, Quasistatic and
Reversible process, Non-equilibrium and Irreversible Processes; Zeroeth Law
and Temperature, First Law and Internal Energy; Second Law - Entropy and
Absolute Temperature; Third Law and Absolute Entropy.
Thermodynamics of simple compressible systems, State postulate, Fundamental
Representations, Thermodynamic Potentials; Jacobean and Legender
Transformations - Maxwell's Equations, Derivation of thermodynamic properties.
Applications: Closed and open systems, Polytropic processes, Cyclic process -
Carnot’s cycle; Gas and vapour power cycles; Mixtures of gases and vapours,
One-D compressible flow, isentropic flow, flow with friction and heat transfer,
supersonic flow and normal shock.
Piston –Prop Engines for Aircraft:
The Otto cycles; IC engines for aircraft application Reciprocating engine
performance; Supercharging and Performance enhancement; Propeller
fundamentals & Theories.

More info

About the teachers

Bhaskar ROY

IIT Bombay

DATE OF JOINING THE INSTITUTE : April, 1985

QUALIFICATION :
B.Tech (Hons.) (Aero.), IIT, Kharagpur- 1973, M.Tech (Aero.), IIT, Bombay 1975 ;
Ph.D. (Engg.), IIT, Kharagpur, 1984

COURSES TAUGHT:
Thermodynamics, Aircraft Propulsion, Aerodynamic Design of Compressors and
Turbines, Aircraft Powerplant Design , Turbomachines

SPECIALIZATION :
A/C Propulsion, Turbomachines, Axial & Centrifugal Flow
Compressor/Fan and Axial Turbine Design

RESEARCH INTERESTS:
a) Cascade Studies of Highly Loaded, Swept, Blade Profiles for Axial Compressor/Fan ;
b) Contra-Rotating Twin Rotor Axial Flow Fans;
c) Casing Boundary Layer Control in Axial Flow Fan/Compressor ;
d) Axial Flow Fan/Compressor Performance with Distortion and Swirl.

Prof. A M Pradeep

Department of Aerospace Engineering, IITB

Awards & Fellowships
Gold medal for the best paper in Aerospace Engineering Division during 2003-2004, by the Institution of Engineers (India)
SAFRAN-French Embassy second prize for the best Ph.D. thesis in Aerospace Engineering published during 2002-2007

2021 Donald Julius Groen Prize from Institution of Mechanical Engineers (IMechE, UK) for the paper: Manas, MP and Pradeep A M, "Stall Inception Mechanisms in a Contra-rotating Fan Operating at Different Speed Combinations", Proc. of IMechE, Part A, Journal of Power and Energy, V234, pp1041-1052. 

Departmental award for excellence in teaching, 2019 & Hotchand & Jamunabhai Lala teaching award, 2019

Prof. S P Sukhatme award for Excellence in Teaching, 2023

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