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

Course Lectures

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

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

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• Mod-01 Lec-03 An introduction to Normal Shocks

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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