ME2351 Gas Dynamics And Jet Propulsion Hand Written Lecture Notes - Kavi Edition

  • 2Jan
  • 2016
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    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.


    CONTENT:
    UNIT-1 (Pages: 32)
    COMPRESSIBLE FLOW
    UNIT-2 (Pages: 26)
    ISENTROFIL FLOWS
    UNIT-3 (Pages: 24)
    GAS DYNAMICS AND JET PROPULSION
    UNIT-4 (Pages: 20)
    JET PROPULSION
    UNIT-5 (Pages: 8)
    SPACE PROPULSION

    Attachment: click here

    UNIT-1
    COMPRESSIBLE FLOW
    BASIC CONCEPTS
    Problems
    To Find
    1. Velocity of sound
    2. Velocity of sound at stagnation condition
    3. Maximum fluid velocity of jet 
    4. Stagnation enthalpy
    5. Crocco number
    To find
    1. Temperature and velocity of gas at exit
    2. Mass flow rate per square metre at inlet cross sectional area
    3. Stagnation temperature
    To find
    1. Mach number and stagnation temperature at exit
    2. Mass flow rate for diameter of 15cm
    3. Exit pressure
    To find
    1. Stagnation temperature
    2. Maximum velocity
    3. Mass flow rate
    4. Area of cross section at entrance
    To find
    1. Mass of air entering in 1 second
    2. Speed of the aircraft 
    3. Stagnation pressure, temperature at diffuser entry
    To find
    1. Sea level where temperature 
    2. Altitude where temperature
    UNIT-2
    ISENTROFIL FLOWS
    To find
    1. Inlet area
    2. Total pressure, total temperature
    3. Exit area and exit static pressure
    To find
    1. What is the shape of the nozzle
    2. The mach number at entry and exit
    To find
    1. Mass flow rate
    2. Properties at exit
    UNIT-3
    GAS DYNAMICS AND JET PROPULSION
    Shock waves
    Full problems

    UNIT-4
    JET PROPULSION
    1. Thrust co.efficient cf.
    2. Propellent weight flow co.efficient cw.
    3. Specific propellent consumption 
    4. Characteristic velocity
    To find
    1. Propulsive power
    2. Thermal efficiency
    3. Propulsive efficiency
    To find
    1. Thrust F
    2. Specific thrust fsp
    To find 
    1. Velocity at exit of the nozzle, cj
    2. Thrust specific fuel consumption
    UNIT-5
    SPACE PROPULSION
    Full Problems


    Attachment: click here