Lecture 31 of 40Advanced Gas Dynamics
Example Problem using Thin Airfoil Theory
Dr. Rinku Mukherjee · IIT Madras
Credits and licence
- From
- Advanced Gas Dynamics, IIT Madras (at NPTEL)
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only.
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
- Tweens profiles and older. How courses are placed
All the lectures
- Introduction to Gas Dynamics & Review of Basic Thermodynamics
- Review of Basic Thermodynamics Continued
- An introduction to Normal Shocks
- The Mach Number and Compressible Flow
- The relation of physical properties across a normal shock
- Normal Shock in a duct: Throat and 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 and 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: Design of a minimum length nozzle
- Application of The Method of Characteristics: Flow through a diverging channel
- 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 and Transformed Coordinate System
- Critical Mach Number and 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
- Supersonic Flow past a 3D Cone at an angle of attack: Flow Visualization - I
- Supersonic Flow past a 3D Cone at an angle of attack: Flow Visualization - II
- 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