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Details
Gas Dynamics and Jet Propulsion Premium Lecture Notes. Specially for Mechanical Engineering Candidates. Syllabus Covered based on Anna University B.E Mechanical Engineering Sixth Semester.
GAS DYNAMICS AND JET PROPULSION
UNIT-1
BASIC CONCEPTS AND ISENTROPIC FLOW
UNIT-2
FLOW THROUGH
UNIT 3
NORMAL AND OBLIQUE SHOCK
UNIT 4
JET PROPULSION
UNIT-5
SPACE PROPULSION
UNIT-1
BASIC CONCEPTS AND ISENTROPIC FLOW
Gas dynamics
Types of fluid flow
Types of system
Energy equation
Momentum equation
Stagnation enthalpy
Stagnation pressure
Stagnation velocity of sound
Stagnation density
Mach wave
Crocco number
Flow in diffuserUNIT-2
FLOW THROUGH
Problems
To determine mass flow rate
To determine inert exit property
Rayleigh flow
ProblemsUNIT 3
NORMAL AND OBLIQUE SHOCK
Shock wave
Normal shock wave
Prandit-Meyer reaction
Problems
Strength of Shock wave
Rainkine Hugnoit EquationUNIT 4
Propulsion device (ENGINES)
Types of Engine
Ramjet Basic Operation
Turbojet Engine
Mass Flow Rate
Schematic Diagram of Turbo Engine
Efficiency Formula for Ramjet
UNIT-5
Problems
Formula for space propulsion
Liquid propellant rocket engine
Gas pressure feed system
Turbo – pump feed system
Solid propellant rocket motor
Hybrid propellant rocket engine - Additional Information
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Additional Information
Pages 196 Author Vinoth Kumar - Reviews
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