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Mechanical Engineering

Advanced Gas Dynamic

Advanced Gas Dynamic

01 Introduction to Gas Dynamics & Review of Basic Thermodynamics

02 Review of Basic Thermodynamics Continued

03 An introduction to Normal Shocks

04 The Mach Number and Compressible Flow-mod01lec04

05 The relation of physical properties across a normal shock-mod01lec05

06 Normal Shock in a duct_ Throat and Reservoir conditions

07 Example Problems in Normal Shocks

08 An introduction to Oblique Shocks

09 The relation of physical properties across an oblique shock

10 Example Problems in Oblique Shocks

11 Pressure - Deflection relationship of Shocks

12 An introduction to Expansion waves

13 Area - Mach Relationship

14 Unsteady Shock Waves_ The Shock Tube

15 The Shock Tube_ Propagating Normal Shock and its reflection from end wall

16 A review of wave propagation

17 Wave propagation_ Small Perturbation Theory

18 Finite Wave Theory_ An introduction to the Method of Characteristics

19 The Shock Tube_ Propagating Expansion Fan

20 The Method of Characteristics

21 Application of The Method of Characteristics_ Design of a minimum length nozzle

22 Application of The Method of Characteristics_ Flow through a diverging channel

23 Flow over a Wavy wall_ Formulation using Perturbation Theory

24 Subsonic Flow over a Wavy wall

25 Supersonic Flow over a Wavy wall

26 Supersonic Flow past a 3D Cone_ Axisymmetric_Quasi 2D Flow

27 Quasi 2D Flow - I

29 Similarity Rules and Transformed Coordinate System

30 Critical Mach Number and Thin Airfoil Theory

31 Example Problem using Thin Airfoil Theory

32 Example Problems

33 Example Problems

34 Example Problems

35 Supersonic Flow past a 3D Cone at an angle of attack

36 Supersonic Flow past a 3D Cone at an angle of attack_ Flow Visualization - I

37 Supersonic Flow past a 3D Cone at an angle of attack_ Flow Visualization - II

38 Supersonic Flow past a 3D Cone at an angle of attack_ Governing Equations

39 Supersonic Flow past a 3D Cone at an angle of attack_ Numerical Procedure

40 Supersonic Flow past a 3D Bluff Body at an angle of attack

28 Quasi 2D Flow - II

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