Advanced Gas Dynamics (USB)

Special Price ₹760.00 Regular Price ₹950.00
In stock
SKU
112106056



Media Storage Type : 32 GB USB Stick

NPTEL Subject Matter Expert : Dr. Rinku Mukherjee

NPTEL Co-ordinating Institute : IIT Madras

NPTEL Lecture Count : 40

NPTEL Course Size : 18 GB

NPTEL PDF Text Transcription : Available and Included

NPTEL Subtitle Transcription : Available and Included (SRT)


Lecture Titles:

Lecture 1 - Introduction to Gas Dynamics & Review of Basic Thermodynamics
Lecture 2 - Review of Basic Thermodynamics Continued
Lecture 3 - An introduction to Normal Shocks
Lecture 4 - The Mach Number and Compressible Flow
Lecture 5 - The relation of physical properties across a normal shock
Lecture 6 - Normal Shock in a duct: Throat and Reservoir conditions
Lecture 7 - Example Problems in Normal Shocks
Lecture 8 - An introduction to Oblique Shocks
Lecture 9 - The relation of physical properties across an oblique shock
Lecture 10 - Example Problems in Oblique Shocks
Lecture 11 - Pressure - Deflection relationship of Shocks
Lecture 12 - An introduction to Expansion waves
Lecture 13 - Area - Mach Relationship
Lecture 14 - Unsteady Shock Waves: The Shock Tube
Lecture 15 - The Shock Tube: Propagating Normal Shock and its reflection from end wall
Lecture 16 - A review of wave propagation
Lecture 17 - Wave propagation: Small Perturbation Theory
Lecture 18 - Finite Wave Theory: An introduction to the Method of Characteristics
Lecture 19 - The Shock Tube: Propagating Expansion Fan
Lecture 20 - The Method of Characteristics
Lecture 21 - Application of The Method of Characteristics: Design of a minimum length nozzle
Lecture 22 - Application of The Method of Characteristics: Flow through a diverging channel
Lecture 23 - Flow over a Wavy wall: Formulation using Perturbation Theory
Lecture 24 - Subsonic Flow over a Wavy wall
Lecture 25 - Supersonic Flow over a Wavy wall
Lecture 26 - Supersonic Flow past a 3D Cone: Axisymmetric/Quasi 2D Flow
Lecture 27 - Quasi 2D Flow - I
Lecture 28 - Quasi 2D Flow - II
Lecture 29 - Similarity Rules and Transformed Coordinate System
Lecture 30 - Critical Mach Number and Thin Airfoil Theory
Lecture 31 - Example Problem using Thin Airfoil Theory
Lecture 32 - Example Problems - 1
Lecture 33 - Example Problems - 2
Lecture 34 - Example Problems - 3
Lecture 35 - Supersonic Flow past a 3D Cone at an angle of attack
Lecture 36 - Supersonic Flow past a 3D Cone at an angle of attack: Flow Visualization - I
Lecture 37 - Supersonic Flow past a 3D Cone at an angle of attack: Flow Visualization - II
Lecture 38 - Supersonic Flow past a 3D Cone at an angle of attack: Governing Equations
Lecture 39 - Supersonic Flow past a 3D Cone at an angle of attack: Numerical Procedure
Lecture 40 - Supersonic Flow past a 3D Bluff Body at an angle of attack

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