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- Advanced Gas Dynamics
Curriculum
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- 40 Lessons
- 10 Weeks
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- Advanced Gas Dynamics40
- 2.1Introduction to Gas Dynamics & Review of Basic Thermodynamics
- 2.2Review of Basic Thermodynamics
- 2.3An Introduction to Normal Shocks
- 2.4The Mach Number & Compressible Flow
- 2.5The Relation of Physical Properties Across a
- 2.6Normal Shock Normal Shock in a Duct: Throat & Reservoir Conditions
- 2.7Example Problems in Normal Shocks
- 2.8An introduction to Oblique Shocks
- 2.9The Relation of Physical Properties Across an Oblique Shock
- 2.10Example Problems in Oblique Shocks
- 2.11Pressure – Deflection Relationship of Shocks
- 2.12An Introduction to Expansion Waves
- 2.13Area – Mach Relationship
- 2.14Unsteady Shock Waves: The Shock Tube
- 2.15The Shock Tube: Propagating Normal Shock & its Reflection from End Wall
- 2.16A Review of Wave Propagation
- 2.17Wave Propagation: Small Perturbation Theory
- 2.18Finite Wave Theory: An Introduction to the Method of Characteristics
- 2.19The Shock Tube: Propagating Expansion Fan
- 2.20The Method of Characteristics
- 2.21Application of the Method of Characteristics-I
- 2.22Application of the Method of Characteristics-II
- 2.23Flow over a Wavy Wall: Formulation using Perturbation Theory
- 2.24Subsonic Flow Over a Wavy Wall
- 2.25Supersonic Flow Over a Wavy Wall
- 2.26Supersonic Flow Past a 3D Cone: Axisymmetric/Quasi 2D Flow
- 2.27Quasi 2D Flow – I
- 2.28Quasi 2D Flow – II
- 2.29Similarity Rules & Transformed Coordinate System
- 2.30Critical Mach Number & Thin Airfoil Theory
- 2.31Example Problem using Thin Airfoil Theory
- 2.32Example Problems – 1
- 2.33Example Problems – 2
- 2.34Example Problems – 3
- 2.35Supersonic Flow Past a 3D Cone at an Angle of Attack-I
- 2.36Supersonic Flow Past a 3D Cone at an Angle of Attack-II
- 2.37Supersonic Flow Past a 3D Cone at an Angle of Attack-III
- 2.38Supersonic Flow Past a 3D Cone at an Angle of Attack: Governing Equations
- 2.39Supersonic Flow Past a 3D Cone at an Angle of Attack: Numerical Procedure
- 2.40Supersonic Flow Past a 3D Bluff Body at an Angle of Attack