Aerospace Structures-II AS 5th Sem Syllabus for VTU BE 2017 Scheme

Aerospace Structures-II detail syllabus for Aerospace Engineering (As), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AS51), 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 as 5th sem syllabus for be 2017 scheme vtu you can visit AS 5th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for aerospace structures-ii is as follows.

Course Objectives:

This course will enable students to

1. Comprehend the basic concepts of theory of bending.
2. Acquire the knowledge of shear flow and buckling.
3. Understand the missile and satellite structures.

Module 1

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Module 2

Shear Flow: Shear stresses in beams – Shear flow in stiffened panels -Shear flow in thin walled open tubes – Shear centre – Shear flow in open sections with stiffeners.

Module 3

Shear Flow Analyses: Shear flow in closed sections with stiffeners-Angle of twist – Shear flow in two flange and three flange box beams -Shear centre – Shear flow in thin walled closed tubes – Bredt-Batho theory – Torsional shear flow in multi cell tubes – Flexural shear flow in multi cell stiffened structures.

Module 4

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Module 5

Launch Vehicle and Spacecraft Structures: Launch vehicle structures – Loads and stresses, thin walled pressure vessels, Buckling of beams, thin wall assumption. spacecraft – mini, micro structures, inflatable structures, flying effector, nanotubing.

Course Outcomes:

After studying this course, students will be able to:

1. Compute the shear flow in open and closed section.
2. Analyze the stability problems of thin walled structures.
3. Distinguish the mini and micro structures.

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:

1. Megson, T.M.G; Aircraft Structures for Engineering Students, ELSEVIER,5th edition,2013,ISBN-13: 978-9382291053.
2. E.F. Bruhn, Analysis and Design of Flight Vehicle Structures, Tristate Offset Co., 1980.

Reference Books:

1. Peery, D.J. and Azar, J.J., Aircraft Structures,McGraw-Hill,New York,2nd Edition,1993.
2. Stephen P. Timoshenko & S.woinowsky Krieger, Theory of Plates and Shells, McGraw-Hill, Singapore,2nd edition, 2010,ISBN-13: 978-0070701250.
3. Rivello, R.M., Theory and Analysis of Flight structures, McGraw-Hill, N.Y., 1993.

For detail syllabus of all other subjects of BE As, 2017 scheme do visit As 5th Sem syllabus for 2017 scheme.

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