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Fundamentals of Gas Dynamics. Instructor: Dr. A. Sameen, Department of Aerospace Engineering, IIT Madras.

FREE
This course includes
Hours of videos

1333 years, 2 months

Units & Quizzes

48

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Certificate of Completion

The course introduces compressible flow and its constitutive equations. The physical concepts behind isentropic flows, area-Mach number relation etc will be discussed with practical problems in mind. Properties of shocks and expansions are important parts of this course. All the numerical examples will be in SI units. (from nptel.ac.in)

Course Currilcum

    • Lecture 01 – Introduction Unlimited
    • Lecture 02 – Basics of Thermodynamics Unlimited
    • Lecture 03 – Tutorial 1 Unlimited
    • Lecture 04 – Control Volume Approach; Reynolds Transport Theorem Unlimited
    • Lecture 05 – Conservation Equations Unlimited
    • Lecture 06 – Tutorial 2 Unlimited
    • Lecture 07 – Energy Equation: Differential Form of Energy Equation, Pressure-Energy Relation Unlimited
    • Lecture 08 – Concept of Stagnation Unlimited
    • Lecture 09 – Discussion on Stagnation Unlimited
    • Lecture 10 – Velocity of Sound Unlimited
    • Lecture 11 – Discussion on Velocity of Sound and Mach Number Unlimited
    • Lecture 12 – Wave Propagation Unlimited
    • Lecture 13 – Mach Wave, Mach Cone, Mach Angle Unlimited
    • Lecture 14 – Mach Number Relations Unlimited
    • Lecture 15 – Variable Area Adiabatic Flow Unlimited
    • Lecture 16 – Variable Area Adiabatic Flow (cont.) Unlimited
    • Lecture 17 – A*, P*, T*, M* Reference Quantities and their Relations Unlimited
    • Lecture 18 – Importance of Stagnation Temperature in Relation to V Unlimited
    • Lecture 19 – Discussion on Variable Area Adiabatic Flow and *Reference Quantities Unlimited
    • Lecture 20 – Use of Gas Tables to Solve the Isentropic Flow Problems Unlimited
    • Lecture 21 – Converging Nozzle Unlimited
    • Lecture 22 – Condition of Choked Flow and Associated Properties Unlimited
    • Lecture 23 – Area Ratio and Pressure Ratio in Converging Nozzles Unlimited
    • Lecture 24 – Discussion on Converging Nozzles Unlimited
    • Lecture 25 – Converging-Diverging Nozzles Unlimited
    • Lecture 26 – More on Converging-Diverging Nozzles Unlimited
    • Lecture 27 – Discussion on Converging-Diverging Nozzles 1 Unlimited
    • Lecture 28 – Discussion on Converging-Diverging Nozzles 2 Unlimited
    • Lecture 29 – Examples and Applications of Flow through Converging-Diverging Nozzles Unlimited
    • Lecture 30 – Introduction to Normal Shocks Unlimited
    • Lecture 31 – Normal Shock Relations 1 Unlimited
    • Lecture 32 – Normal Shock Relations 2 Unlimited
    • Lecture 33 – Rankine-Hugoniot Equation Unlimited
    • Lecture 34 – Discussion on Normal Shocks 1 Unlimited
    • Lecture 35 – Discussion on Normal Shocks 2 Unlimited
    • Lecture 36 – Normal Shocks in Converging-Diverging Nozzles Unlimited
    • Lecture 37 – Normal Shocks in Converging-Diverging Nozzles (cont.) Unlimited
    • Lecture 38 – Moving Normal Shocks Unlimited
    • Lecture 39 – Discussion on Moving Normal Shocks Unlimited
    • Lecture 40 – Oblique Shocks Unlimited
    • Lecture 41 – Oblique Shock Relations Unlimited
    • Lecture 42 – Discussion on Oblique Shocks Unlimited
    • Lecture 43 – Shock Polar Diagram and Prandtl-Meyer Relation for Oblique Shocks Unlimited
    • Lecture 44 – Reflection of Oblique Shocks Unlimited
    • Lecture 45 – Discussion on Reflection of Oblique Shocks Unlimited
    • Lecture 46 – Prandtl-Meyer Flow Unlimited
    • Lecture 47 – Prandtl-Meyer Flow (cont.) Unlimited
    • Lecture 48 – Discussion on Prandtl-Meyer Expansion Unlimited