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ASE202 — Propulsion-I

Practice

Course Overview

ASE202 3 Credits L:3 T:0 P:0
Download Syllabus

This course covers gas turbine engines and their components, subsonic and supersonic inlets, axial-flow and centrifugal compressors, combustion chambers, and elementary turbine design and performance.

Study Units

Unit 1

Fundamentals of Gas Turbine

Notes MCQ Subjective
Unit 2

Inlets

Notes MCQ Subjective
Unit 3

Axial Flow Compressors

Notes MCQ Subjective
Unit 4

Centrifugal Compressors

Notes MCQ Subjective
Unit 5

Combustion Chambers

Notes MCQ Subjective
Unit 6

Elementary Turbine Design

Notes MCQ Subjective

Continuous Assessment

3 components

Best 2 of 3 CAs will be considered for evaluation.
Test 1 50%

Written exam unit 1, 2 and 3 (partially)

Week 3 / 4

Rubric
To recall the basics of Gas turbine engines, operating principal of subsonic and Supersonic inlets

Test 2 50%

Written exam units 4,5 and 6

Week 9 / 10

Rubric
To compute the concepts of axial flow compressors and their performance characteristics

Test 3 50%

Written exam with syllabus that was covered for CA 1 and CA 2

Week 11 / 12

Rubric
To test the knowledge of the students and give them an opportunity to improve their CA scores

Exams & Practice

Mid Term Examination

Mid-semester comprehensive evaluation

20%

End Term Examination

Final semester comprehensive evaluation

50%

Type: Examination

ASE202 - FAQs

How many units are in ASE202?

ASE202 has 6 units. Each unit includes detailed notes and MCQ practice questions.

What exam resources are available for ASE202?

Unit-wise notes and MCQ practice are available. Exam resources coming soon.

How to prepare for ASE202 exams?

Study each unit's notes thoroughly, practice MCQs to test understanding, and attempt mock tests before exams. Focus on important topics and previous year questions.