About Course
Welcome to the Complete Gas Dynamics Lecture Series for GATE Aerospace 2027 aspirants! This comprehensive series consists of 31 premium lectures, meticulously designed to cover the entire syllabus of Gas Dynamics (Compressible Flows) for the GATE Aerospace exam. Each lecture provides a blend of theoretical explanations, real-world applications, and detailed numerical problem-solving sessions to ensure a deep understanding of every topic.
Whether you’re a beginner or revising for the exam, this series will guide you through all the key concepts, including:
- Isentropic flows
- Normal and oblique shock waves
- Prandtl-Meyer expansion
- Rayleigh and Fanno flows
- Area-Mach number relations
- Choking and nozzle flows
- Reservoir conditions and more
These lectures are accessible to all GATE Aerospace aspirants. The content has been structured to provide step-by-step clarity, helping students excel in one of the most critical subjects for the GATE Aerospace exam.
Take advantage of this resource and boost your preparation!
- Gas Dynamics for GATE Aerospace
- GATE Aerospace Gas Dynamics Free Lectures
- Compressible Flows Lecture Series
- Gas Dynamics Numerical Solving GATE 2025
- Shock Waves GATE Aerospace
- Fanno Flow and Rayleigh Flow GATE
- Isentropic Flow Lectures
- Free GATE Aerospace Study Material
Course Content
Gas Dynamics
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Must Watch Before Starting the Course | GATE Aerospace Learning
01:45 -
Lecture 1 – Complete GD Syllabus Discussion
12:46 -
20:46
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Lecture 3_ Incompressible vs Compressible Flow, Flow Regimes & Mach Number
15:09 -
Lecture 4_ Numerical – 01
11:51 -
Lecture 5_ Isentropic Flow, Isentropic Relations & Stagnation Properties
23:24 -
Lecture 6_ Area-Velocity Relation & Numerical – 02
39:29 -
Lecture 7 _ Flow Through C-D Duct, Choking & Area Mach Number Relation
34:20 -
Lecture 8 _ Mass Flow Rate & Characteristics Mach Number
54:38 -
40:44
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Lecture 10 _ Moving Normal Shock Wave With Numerical
01:21:34 -
Lecture 11 _ Oblique Shock Wave
29:33 -
Lecture 12 – Theta-Beta-Mach relation Part 01
26:12 -
Lecture 13 _ Theta-Beta-Mach relation Part 02
24:23 -
Lecture 14 _ Numerical Solving _Isentropic Relations, Nozzle Flows & Standing NSW
48:36 -
Lecture 15 _ Numerical Solving – 02 _ Area Mach Number Relation, C-D nozzle with Wind Tunnel
30:49 -
Lecture 16 _ Numerical Solving – 03 _ Oblique Shock Waves (Graphical & Numerical)
21:18 -
Lecture 17 _ PRANDTL-MEYER EXPANSION FAN & ISENTROPIC COMPRESSION & NUMERICAL
34:06 -
Lecture 18_ Effect of Back Pressure on C-D Nozzle _ Underexpansion & Overexpansion
46:38 -
Lecture 19 _ Detached Shock Wave, Rayleigh Supersonic Pitot Formula
37:18 -
Lecture 20 _ Rayleigh Flow, Fanno Flow & Supersonic Wind Tunnel
59:29 -
Lecture 21 _ Shock Reflection & Intersection in Gas Dynamics
13:50 -
Lecture 22 _ Numerical Solving Session – 02 Basics & Isentropic Flows
52:28 -
Lecture 23_ Numerical Solving Session 3
55:32 -
Lecture 24_ Numerical Solving Session 4 _ Area Velocity Relation, Oblique Shock Wave, Expansion Fan
44:30 -
Lecture 25_ Numerical Solving Session 5 _ Area Velocity Relation, Oblique Shock Wave, Expansion Fan
38:16 -
Lecture 26_ Numerical Solving Session 6 – Normal Shock Wave
37:03 -
Lecture 27_ Numerical Solving Session 7
28:44 -
Lecture 28_ Numerical Solving Session 08
42:22 -
Lecture 29 _ Numerical Solving Session 9 _ Rayleigh Flow & Fanno Flow
32:14 -
Lecture 30 _ Numerical Solving Session-10 _ Rayleigh Flow & Oblique Shock Wave
15:48 -
Lecture 31 _ Rocket Engine Nozzle Numerical _ Thrust & Exit Area Calculation with Gas Dynamics
31:39
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