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Mod-01 Lec-01 Lecture-01-Introduction to Gas Dynamics & Review of Basic Thermodynamics

Mod-01 Lec-02 Lecture-02-Review of Basic Thermodynamics Continued

Mod-01 Lec-03 An introduction to Normal Shocks

Mod-01 Lec-04 Lecture-04-The Mach Number and Compressible Flow

Mod-01 Lec-05 Lecture-05-The relation of physical properties across a normal shock

Mod-01 Lec-06 Lecture-06-Normal Shock in a duct: Throat and Reservoir conditions

Mod-01 Lec-07 Lecture-07-Example Problems in Normal Shocks

Mod-01 Lec-08 Lecture-08-An introduction to Oblique Shocks

Mod-01 Lec-09 The relation of physical properties across an oblique shock

Mod-01 Lec-10 Lecture-10-Example Problems in Oblique Shocks

Mod-01 Lec-11 Lecture-11-Pressure - Deflection relationship of Shocks

Mod-01 Lec-12 Lecture-12-An introduction to Expansion waves

Mod-01 Lec-13 Lecture-13-Area - Mach Relationship

Mod-01 Lec-14 Lecture-14-Unsteady Shock Waves: The Shock Tube

Mod-01 Lec-15 Lecture-15-The Shock Tube: Propagating Normal Shock and its reflection from end wall

Mod-01 Lec-16 Lecture-16-A review of wave propagation

Mod-01 Lec-17 Lecture-17-Wave propagation: Small Perturbation Theory

Mod-01 Lec-18 Lecture-18-Finite Wave Theory: An introduction to the Method of Characteristics

Mod-01 Lec-19 Lecture-19-The Shock Tube: Propagating Expansion Fan

Mod-01 Lec-20 Lecture-20-The Method of Characteristics

Mod-01 Lec-21 Lecture-21-Application of The Method of Characteristics:

Mod-01 Lec-22 Lecture-22-Application of The Method of Characteristics:

Mod-01 Lec-23 Lecture-23-Flow over a Wavy wall: Formulation using Perturbation Theory

Mod-01 Lec-24 Lecture-24-Subsonic Flow over a Wavy wall

Mod-01 Lec-25 Lecture-25-Supersonic Flow over a Wavy wall

Mod-01 Lec-26 Lecture-26-Supersonic Flow past a 3D Cone: Axisymmetric/Quasi 2D Flow

Mod-01 Lec-27 Lecture-27-Quasi 2D Flow - I

Mod-01 Lec-28 Lecture-28-Quasi 2D Flow - II

Mod-01 Lec-29 Similarity Rules and Transformed Coordinate System

Mod-01 Lec-30 Lecture-30-Critical Mach Number and Thin Airfoil Theory

Mod-01 Lec-31 Lecture-31-Example Problem using Thin Airfoil Theory

Mod-01 Lec-32 Lecture-32-Example Problems - 1

Mod-01 Lec-33 Lecture-33-Example Problems - 2

Mod-01 Lec-34 Lecture-34-Example Problems - 3

Mod-01 Lec-35 Lecture-35-Supersonic Flow past a 3D Cone at an angle of attack

Mod-01 Lec-36 Lecture-36-Supersonic Flow past a 3D Cone at an angle of attack:

Mod-01 Lec-37 Lecture-37-Supersonic Flow past a 3D Cone at an angle of attack:

Mod-01 Lec-38 Supersonic Flow past a 3D Cone at an angle of attack: Governing Equations

Mod-01 Lec-39 Supersonic Flow past a 3D Cone at an angle of attack: Numerical Procedure

Mod-01 Lec-40 Supersonic Flow past a 3D Bluff Body at an angle of attack

Description:

Instructor: Dr. Rinku Mukherjee, Department of Applied Mechanics, IIT Madras. This course introduces the concepts of the primary differences between an incompressible flow and a compressible flow. It draws the connection between compressible flow and speed of sound, Mach Number and thermodynamics. It then builds on the governing equations to derive the commonly known equations and tackles both 2D and 3D problems. The physical concept of shocks and the resulting changes in the thermodynamic properties of a fluid form a major part of this course. The course concentrates primarily on the understanding of the physical concepts of compressible flow and keeps a reference to various numerical methods for solving the governing equations to a minimum.

Advanced Gas Dynamics

NPTEL

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#Engineering #Mechanical Engineering #Science #Physics #Thermodynamics #Fluid Mechanics #Fluid Dynamics #Shock Waves #Compressible Flow #Wave Propagation #Gas Dynamics

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