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# Gas Dynamics And Jet Propulsion Premium Lecture Notes(Problems) - Kavi Edition

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Gas Dynamics And Jet Propulsion Premium Lecture Notes(Problems) - Kavi Edition
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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

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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.

GAS DYNAMICS
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

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