Please use this identifier to cite or link to this item: http://doer.col.org/handle/123456789/2267
Title: Advanced Gas Dynamics
Authors: Mukherjee, R. (Rinku)
Keywords: mechanical engineering
mechanics & thermodynamics
Edutags: Full Course
Postgraduate
Issue Date: Apr-2013
Publisher: National Programme on Technology Enhanced Learning (NPTEL)
Abstract: Modules / Lectures : Introduction to Gas Dynamics & Review of Basic Thermodynamics ; 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 ; Similarity Rules and Transformed Coordinate System ; Critical Mach Number and Thin Airfoil Theory ; Example Problem using Thin Airfoil Theory ; Supersonic Flow past a 3D Cone at an angle of attack ; Supersonic Flow past a 3D Cone at an angle of attack: Flow Visualization ; 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 ;
Original Source: http://nptel.ac.in/courses/112106056/
Appears in Collections:Natural & Life Sciences

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