Advanced Gas Dynamics

Introduction to Gas Dynamics & Review of Basic Thermodynamics

Review of Basic Thermodynamics

An Introduction to Normal Shocks

The Mach Number & Compressible Flow

The Relation of Physical Properties Across a

Normal Shock Normal Shock in a Duct: Throat & Reservoir Conditions

Example Problems in Normal Shocks

An introduction to Oblique Shocks

The Relation of Physical Properties Across an Oblique Shock

Example Problems in Oblique Shocks

Pressure – Deflection Relationship of Shocks

An Introduction to Expansion Waves

Area – Mach Relationship

Unsteady Shock Waves: The Shock Tube

The Shock Tube: Propagating Normal Shock & its Reflection from End Wall

A Review of Wave Propagation

Wave Propagation: Small Perturbation Theory

Finite Wave Theory: An Introduction to the Method of Characteristics

The Shock Tube: Propagating Expansion Fan

The Method of Characteristics

Application of the Method of Characteristics-I

Application of the Method of Characteristics-II

Flow over a Wavy Wall: Formulation using Perturbation Theory

Subsonic Flow Over a Wavy Wall

Supersonic Flow Over a Wavy Wall

Supersonic Flow Past a 3D Cone: Axisymmetric/Quasi 2D Flow

Quasi 2D Flow – I

Quasi 2D Flow – II

Similarity Rules & Transformed Coordinate System

Critical Mach Number & Thin Airfoil Theory

Example Problem using Thin Airfoil Theory

Example Problems – 1

Example Problems – 2

Example Problems – 3

Supersonic Flow Past a 3D Cone at an Angle of Attack-I

Supersonic Flow Past a 3D Cone at an Angle of Attack-II

Supersonic Flow Past a 3D Cone at an Angle of Attack-III

Supersonic Flow Past a 3D Cone at an Angle of Attack: Governing Equations

Supersonic Flow Past a 3D Cone at an Angle of Attack: Numerical Procedure

Supersonic Flow Past a 3D Bluff Body at an Angle of Attack