Aero-Elasticity detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AE744), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.
For all other aero 7th sem syllabus for be 2017 scheme vtu you can visit Aero 7th Sem syllabus for BE 2017 Scheme VTU Subjects. For all other Professional Elective-3 subjects do refer to Professional Elective-3. The detail syllabus for aero-elasticity is as follows.
Course Objectives:
This course will enable students to
- Understand the basic aero elastic phenomena.
- Comprehend the steady state aero elastic problems and flutter phenomena.
- Acquire the knowledge on the aero elastic problems.
Revised Modules Teaching Bloom’s
Hours Taxonomy (RBT) Level
Module 1
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Module 2
Divergence of a Lifting Surface: Simple two dimensional idealizations -Strip theory – Integral equation of the second kind – Exact solutions for simple rectangular wings – Semi rigid’ assumption and approximate solutions -Generalized coordinates – Successive approximations – Numerical approximations using matrix equations.
Module 3
Steady State Aeroelastic Problems: Loss and reversal of aileron control – Critical aileron reversal speed – Aileron efficiency – Semi rigid theory and successive approximations – Lift distribution – Rigid and elastic wings. Tail efficiency. Effect of elastic deformation on static longitudinal stability.
Module 4
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Module 5
Examples of Aeroelastic Problems: Galloping of transmission lines and Flow induced vibrations of transmission lines, tall slender structures and suspension bridges.
Course Outcomes:
After studying this course, students will be able to:
- Apply the aero elastic phenomena.
- Evaluate the steady state aero elastic problems and flutter phenomena.
- Classify the types of aero elastic problems.
Graduate Attributes (as per NBA):
- Engineering Knowledge.
- Problem Analysis.
- Design / development of solutions
- Interpretation of data
Question paper pattern:
- The question paper will have ten questions.
- Each full question consists of 16 marks.
- There will be 2 full questions (with a maximum of four sub questions) from each module.
- Each full question will have sub questions covering all the topics under a module.
- The students will have to answer 5 full questions, selecting one full question from each module.
Text Books:
- Y.C. Fung, An Introduction to the Theory of Aeroelasticity, Dover Publications Inc, 2008, ISBN-13: 978-0486469362
- E.G. Broadbent, Elementary Theory of Aeroelasticity, Bun Hill Publications Ltd., 1986
Reference Books:
- R.L. Bisplinghoff, H. Ashley, and R.L. Halfmann, Aeroelasticity, II Edition Addison Wesley Publishing Co., Inc., 1996.
- R.H. Scanlan and R. Rosenbaum, Introduction to the study of Aircraft Vibration and Flutter, Macmillan Co., New York, 1981.
- R.D. Blevins, Flow Induced Vibrations, Krieger Pub Co., 2001
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 7th Sem syllabus for 2017 Regulation.
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