Rinku Mukherjee: Advanced Gas Dynamics (IIT Madras)

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source: nptelhrd    2012年7月20日
Mechanical - Advanced Gas Dynamics by Dr. Rinku Mukherjee, Department of Applied Mechanics, IIT Madras. For more details on NPTEL visit http://nptel.iitm.ac.in

01-Introduction to Gas Dynamics & Review of Basic Thermodynamics 50:36
02-Review of Basic Thermodynamics Continued 48:41
03 An introduction to Normal Shocks 48:18
04-The Mach Number and Compressible Flow 49:29
05-The relation of physical properties across a normal shock 51:18
06-Normal Shock in a duct: Throat and Reservoir conditions 48:10
07-Example Problems in Normal Shocks 47:16
08-An introduction to Oblique Shocks 51:02
09 The relation of physical properties across an oblique shock 50:12
10-Example Problems in Oblique Shocks 52:26
11-Pressure - Deflection relationship of Shocks 50:34
12-An introduction to Expansion waves 44:27
13-Area - Mach Relationship 47:11
14-Unsteady Shock Waves: The Shock Tube 51:53
15-The Shock Tube: Propagating Normal Shock and its reflection from end wall 50:47
16-A review of wave propagation 57:23
17-Wave propagation: Small Perturbation Theory 50:30
18-Finite Wave Theory: An introduction to the Method of Characteristics 50:24
19-The Shock Tube: Propagating Expansion Fan 49:55
20-The Method of Characteristics 52:19
21-Application of The Method of Characteristics: 50:44
22-Application of The Method of Characteristics: 50:07
23-Flow over a Wavy wall: Formulation using Perturbation Theory 51:11
24-Subsonic Flow over a Wavy wall 50:46
25-Supersonic Flow over a Wavy wall 49:58
26-Supersonic Flow past a 3D Cone: Axisymmetric/Quasi 2D Flow 48:59
27-Quasi 2D Flow - I 50:49
28-Quasi 2D Flow - II 50:57
29 Similarity Rules and Transformed Coordinate System 49:11
30-Critical Mach Number and Thin Airfoil Theory 50:08
31-Example Problem using Thin Airfoil Theory 43:37
32-Example Problems - 1 52:29
33-Example Problems - 2 49:19
34-Example Problems - 3 53:02
35-Supersonic Flow past a 3D Cone at an angle of attack 49:40
36-Supersonic Flow past a 3D Cone at an angle of attack: 51:40
37-Supersonic Flow past a 3D Cone at an angle of attack: 46:38
38 Supersonic Flow past a 3D Cone at an angle of attack: Governing Equations 51:44
39 Supersonic Flow past a 3D Cone at an angle of attack: Numerical Procedure 50:23
40 Supersonic Flow past a 3D Bluff Body at an angle of attack 52:01