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ME-343: Compressible-fluid dynamics
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Lectures in this course (58)
Straight Shocks in Perfect Gases
Explains shock Mach number, energy conservation, and density ratio in perfect gases.
Straight Shocks: General Equations
Discusses mass, momentum, and energy conservation in straight shock waves.
Straight Shock Waves: Basics
Covers the basics of straight shock waves, including generation, parameters, and observer's frame of reference.
Untitled
Oblique Shock Waves: Graph
Explores oblique shock waves, deflection angles, and explicit relationships for angles.
Oblique Shock Waves in Perfect Gases
Covers relationships in oblique shock waves for perfect gases and their resolution procedures.
Shock Waves: Oblique Shock Theory
Explores the classification and characteristics of oblique shock waves and integral formulations for conservation laws.
Supersonic Nozzles: Wake Effects
Explores the wake effects of supersonic nozzles in different expansion conditions and their impact on thrust.
Prandtl-Meyer Flows: Aero
Explores lift and drag forces, supersonic flow, and wave drag in Prandtl-Meyer flows.
Flow PM Evaluation Table
Presents a table for evaluating the Prandtl-Meyer function based on Mach number.
Prandtl-Meyer Flows: Theory
Explores Prandtl-Meyer flows, focusing on speed variations and the Prandtl-Meyer function's analytical derivation for isentropic waves.
PM Flows: Existence
Covers the existence of strong and weak solutions in PM flows and the behavior of shock waves.
PM Flows: Direction Changes and Shocks
Explores compressible flows, Mach number, pressure, temperature variations, and shock waves.
Characteristics: Examples
Covers the characteristics of a simple region along with examples and resolution methods.
Flow Characteristics - Resolution Method
Covers the method to find flow characteristics in a system.
Flow Characteristics and Equations
Covers the characteristics and equations related to flow in non-viscous fluids, including mass conservation and momentum conservation.
Characteristics - Natural Coordinates
Explores two-dimensional supersonic flows using natural coordinates based on streamlines and normal families, emphasizing their practical applications.
Characteristics: Introduction
Introduces the characteristics of supersonic flows and the conditions for considering irrotational flows.
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