Advanced Gas Dynamics

Advanced Gas Dynamics

nptelhrd via YouTube Direct link

Mod-01 Lec-32 Lecture-32-Example Problems - 1

32 of 40

32 of 40

Mod-01 Lec-32 Lecture-32-Example Problems - 1

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Advanced Gas Dynamics

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

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