Lecture 9 _ Standing Normal Shock Wave – Gate Aerospace Learning

Course Content

Gas Dynamics

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Must Watch Before Starting the Course | GATE Aerospace Learning

Lecture 1 – Complete GD Syllabus Discussion

Lecture 2 – Basics & Isentropic Flows

Lecture 3_ Incompressible vs Compressible Flow, Flow Regimes & Mach Number

Lecture 4_ Numerical – 01

Lecture 5_ Isentropic Flow, Isentropic Relations & Stagnation Properties

Lecture 6_ Area-Velocity Relation & Numerical – 02

Lecture 7 _ Flow Through C-D Duct, Choking & Area Mach Number Relation

Lecture 8 _ Mass Flow Rate & Characteristics Mach Number

Lecture 9 _ Standing Normal Shock Wave

Lecture 10 _ Moving Normal Shock Wave With Numerical

Lecture 11 _ Oblique Shock Wave

Lecture 12 – Theta-Beta-Mach relation Part 01

Lecture 13 _ Theta-Beta-Mach relation Part 02

Lecture 14 _ Numerical Solving _Isentropic Relations, Nozzle Flows & Standing NSW

Lecture 15 _ Numerical Solving – 02 _ Area Mach Number Relation, C-D nozzle with Wind Tunnel

Lecture 16 _ Numerical Solving – 03 _ Oblique Shock Waves (Graphical & Numerical)

Lecture 17 _ PRANDTL-MEYER EXPANSION FAN & ISENTROPIC COMPRESSION & NUMERICAL

Lecture 18_ Effect of Back Pressure on C-D Nozzle _ Underexpansion & Overexpansion

Lecture 19 _ Detached Shock Wave, Rayleigh Supersonic Pitot Formula

Lecture 20 _ Rayleigh Flow, Fanno Flow & Supersonic Wind Tunnel

Lecture 21 _ Shock Reflection & Intersection in Gas Dynamics

Lecture 22 _ Numerical Solving Session – 02 Basics & Isentropic Flows

Lecture 23_ Numerical Solving Session 3

Lecture 24_ Numerical Solving Session 4 _ Area Velocity Relation, Oblique Shock Wave, Expansion Fan

Lecture 25_ Numerical Solving Session 5 _ Area Velocity Relation, Oblique Shock Wave, Expansion Fan

Lecture 26_ Numerical Solving Session 6 – Normal Shock Wave

Lecture 27_ Numerical Solving Session 7

Lecture 28_ Numerical Solving Session 08

Lecture 29 _ Numerical Solving Session 9 _ Rayleigh Flow & Fanno Flow

Lecture 30 _ Numerical Solving Session-10 _ Rayleigh Flow & Oblique Shock Wave

Lecture 31 _ Rocket Engine Nozzle Numerical _ Thrust & Exit Area Calculation with Gas Dynamics

Gas Dynamics/Compressible Flows

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