Aerospace - Introduction to Propulsion | EveryEng

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Self-paced Advanced

Aerospace - Introduction to Propulsion

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11 enrolled

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FREE

2019 min

Anytime

English

1103 views

Saurabh Kumar GuptaMechanical Engineer

Mechanical Engineering

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Why enroll

Completing the 'Aerospace - Introduction to Propulsion' course can significantly enhance your career prospects in the aerospace industry. With a solid understanding of propulsion systems, you'll be well-positioned for roles such as Aerospace Engineer, Propulsion Systems Engineer, or Research and Development Engineer. You'll also be competitive for careers in related fields like defense, automotive, and energy. Additionally, this course provides a foundation for advanced studies or certifications in aerospace engineering, leading to senior roles like Technical Lead, Systems Engineer, or Program Manager. Unlock new opportunities and propel your career forward with this comprehensive introduction to propulsion systems.

Your instructor

Saurabh Kumar Gupta

Content Manager

Mechanical Engineer

5+ yrs experience·India

Is this course for you?

You should take this if

You work in Aerospace
You're a Mechanical Engineering professional
You have 3+ years of hands-on experience in this field
You prefer self-paced learning you can revisit

You should skip if

You're new to this field with no prior experience
You need a different specialisation outside Mechanical Engineering
You need live interaction with an instructor

Course details

This course provides a comprehensive introduction to the fundamentals of propulsion systems used in aerospace engineering. Students will learn about the principles of propulsion, types of propulsion systems, and their applications in aircraft, spacecraft, and missiles.

Source: nptelhrd (YouTube Channel)
Introduction to Propulsion by Dr. D.P. Mishra, Department of Aerospace Engineering, IIT Kanpur.

Course suitable for

Key topics covered

- Understand the fundamental principles of propulsion and thrust

- Identify and describe different types of propulsion systems

- Analyze the performance of propulsion systems

- Apply propulsion concepts to real-world aerospace applications

- Stay updated with the latest developments in propulsion technology

Course content

The course is readily available, allowing learners to start and complete it at their own pace.

40 lectures33 hr 39 min

What do you mean by propulsion ?
45 min
First Flight of Powered Aircraft
45 min
Scramjet Engine
51 min
Laws of thermodynamics
67 min
Continumm in fluid mechanics
55 min
Stream lines and path lines
49 min
Compressible fluid flow
51 min
Flow regimes
57 min
Stagnation Point
49 min
Characteristics of Mach Number
53 min
Convergent Nozzle
49 min
What do you mean by shocks?
53 min
Oblique Shocks
49 min
Example
48 min
Constant Area 1D Flow With Friction
50 min
Combustion
47 min
Chemical Analysis
52 min
Adiabatic Flame temperature
54 min
Procedure of Determining Equilibrium Composition
49 min
Various Combustion Modes
52 min
Analysis of ID Combustion Wave
54 min
Structure of ID Premixed Flame
57 min
Flame thickness
52 min
Minimum Ignition Energy
53 min
Phenomenological Analysis
42 min
Engine Performance Parameters
42 min
Air Breathing Engine Cycle
57 min
Ramjet Engine
43 min
Summary - Ramjet Engine Analysis
56 min
Turbofans
51 min
Types of turbofan configuration
54 min
Real Cycle Analysis
44 min
Turbojet Engines
47 min
Examples
41 min
Turboprep Engines
49 min
Chemically Powered Rocket Engines
51 min
Fundamentals of Aerospace Propulsion
40 min
Solid Propellants
55 min
Types of Solid Propellant Engines
50 min
Atomization
56 min

Opportunities that await you!

Career opportunities

✎ Where this fits — what comes before, what comes next

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Questions and Answers

Q: You're stuck on the hangar floor searching "estimate turbojet thrust from mass flow and exhaust velocity". A small turbojet passes 20 kg/s of air. Exhaust jet velocity relative to the aircraft is about 600 m/s. Inlet velocity is negligible. What thrust order makes sense?

A: The right choice lands the momentum balance in the correct decade: 20 kg/s times 600 m/s gives 12,000 N. B invents losses larger than the momentum term. C confuses energy addition with momentum multiplication. D drops mass flow with no physical basis.

Q: You're reviewing a materials note after googling "gas turbine exhaust corrosion sulfur marine environment". A small turboprop operates from a coastal base, burning fuel with trace sulfur. Exhaust duct skin runs at 500°C. What degradation mechanism dominates?

A: The correct pick targets the temperature–chemistry pairing that attacks alloys in exhaust flow. B applies to wetted joints, not hot gas paths. C needs hydrogen charging conditions that aren't present here. D mislabels a thermal environment with minimal cycling.

Q: During an AOG discussion someone searches "FAA Part 33 engine test overspeed margin why required". A turbine rotor is demonstrated at 110% rated speed during certification. What safety intent drives that requirement?

A: The correct answer ties overspeed testing to containment risk when controls fail. B is covered by separate vibration surveys. C confuses structural demonstration with performance credit. D addresses build variability, not catastrophic rotor release.

Q: Maintenance is referencing "engine fire detection loop failure what still burns". An engine nacelle fire loop goes open-circuit in flight. What does that safeguard failure not prevent?

A: The right choice isolates the physical outcome the loop can't stop: fuel keeps flowing without crew action. B is the opposite failure mode. C sits outside the system boundary. D belongs to engine control and cooling, not fire detection.