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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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Classroom Contents
Advanced Gas Dynamics
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- 1 Mod-01 Lec-01 Lecture-01-Introduction to Gas Dynamics & Review of Basic Thermodynamics
- 2 Mod-01 Lec-02 Lecture-02-Review of Basic Thermodynamics Continued
- 3 Mod-01 Lec-03 An introduction to Normal Shocks
- 4 Mod-01 Lec-04 Lecture-04-The Mach Number and Compressible Flow
- 5 Mod-01 Lec-05 Lecture-05-The relation of physical properties across a normal shock
- 6 Mod-01 Lec-06 Lecture-06-Normal Shock in a duct: Throat and Reservoir conditions
- 7 Mod-01 Lec-07 Lecture-07-Example Problems in Normal Shocks
- 8 Mod-01 Lec-08 Lecture-08-An introduction to Oblique Shocks
- 9 Mod-01 Lec-09 The relation of physical properties across an oblique shock
- 10 Mod-01 Lec-10 Lecture-10-Example Problems in Oblique Shocks
- 11 Mod-01 Lec-11 Lecture-11-Pressure - Deflection relationship of Shocks
- 12 Mod-01 Lec-12 Lecture-12-An introduction to Expansion waves
- 13 Mod-01 Lec-13 Lecture-13-Area - Mach Relationship
- 14 Mod-01 Lec-14 Lecture-14-Unsteady Shock Waves: The Shock Tube
- 15 Mod-01 Lec-15 Lecture-15-The Shock Tube: Propagating Normal Shock and its reflection from end wall
- 16 Mod-01 Lec-16 Lecture-16-A review of wave propagation
- 17 Mod-01 Lec-17 Lecture-17-Wave propagation: Small Perturbation Theory
- 18 Mod-01 Lec-18 Lecture-18-Finite Wave Theory: An introduction to the Method of Characteristics
- 19 Mod-01 Lec-19 Lecture-19-The Shock Tube: Propagating Expansion Fan
- 20 Mod-01 Lec-20 Lecture-20-The Method of Characteristics
- 21 Mod-01 Lec-21 Lecture-21-Application of The Method of Characteristics:
- 22 Mod-01 Lec-22 Lecture-22-Application of The Method of Characteristics:
- 23 Mod-01 Lec-23 Lecture-23-Flow over a Wavy wall: Formulation using Perturbation Theory
- 24 Mod-01 Lec-24 Lecture-24-Subsonic Flow over a Wavy wall
- 25 Mod-01 Lec-25 Lecture-25-Supersonic Flow over a Wavy wall
- 26 Mod-01 Lec-26 Lecture-26-Supersonic Flow past a 3D Cone: Axisymmetric/Quasi 2D Flow
- 27 Mod-01 Lec-27 Lecture-27-Quasi 2D Flow - I
- 28 Mod-01 Lec-28 Lecture-28-Quasi 2D Flow - II
- 29 Mod-01 Lec-29 Similarity Rules and Transformed Coordinate System
- 30 Mod-01 Lec-30 Lecture-30-Critical Mach Number and Thin Airfoil Theory
- 31 Mod-01 Lec-31 Lecture-31-Example Problem using Thin Airfoil Theory
- 32 Mod-01 Lec-32 Lecture-32-Example Problems - 1
- 33 Mod-01 Lec-33 Lecture-33-Example Problems - 2
- 34 Mod-01 Lec-34 Lecture-34-Example Problems - 3
- 35 Mod-01 Lec-35 Lecture-35-Supersonic Flow past a 3D Cone at an angle of attack
- 36 Mod-01 Lec-36 Lecture-36-Supersonic Flow past a 3D Cone at an angle of attack:
- 37 Mod-01 Lec-37 Lecture-37-Supersonic Flow past a 3D Cone at an angle of attack:
- 38 Mod-01 Lec-38 Supersonic Flow past a 3D Cone at an angle of attack: Governing Equations
- 39 Mod-01 Lec-39 Supersonic Flow past a 3D Cone at an angle of attack: Numerical Procedure
- 40 Mod-01 Lec-40 Supersonic Flow past a 3D Bluff Body at an angle of attack
