Hypersonics AS 6th Sem Syllabus for VTU BE 2017 Scheme (Professional Elective-2)

Hypersonics detail syllabus for Aerospace Engineering (As), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AS651), 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 6th sem syllabus for be 2017 scheme vtu you can visit AS 6th Sem syllabus for BE 2017 Scheme VTU Subjects. For all other Professional Elective-2 subjects do refer to Professional Elective-2. The detail syllabus for hypersonics is as follows.

Course Objectives:

This course will enable students to

1. Understand the basics of hypersonic flows.
2. Understand the approximate methods for inviscid hypersonic flows.
3. Acquire the knowledge of viscous interactions in hypersonic flows.

Module 1

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Module 2

Surface Inclination Methods For Hypersonic Inviscid Flows: Local surface inclination methods, modified Newtonian Law, Newtonian theory – tangent wedge or tangent cone and shock expansion methods, Calculation of surface flow properties.

Module 3

Approximate Methods For Inviscid Hypersonic Flows: Approximate methods hypersonic small disturbance equation and theory, thin shock
layer theory , blast wave theory, entropy effects, rotational method of characteristics, hypersonic shock wave shapes and correlations

Module 4

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Module 5

Viscous Interactions In Hypersonic Flows: Strong and weak viscous interactions, hypersonic shockwaves and boundary layer interactions, Estimation of hypersonic boundary layer transition, Role of similarity parameter for laminar viscous interactions in hypersonic viscous flow.

Course Outcomes:

After studying this course, students will be able to:

1. Apply the basics of hypersonic flows.
2. Apply the approximate methods for inviscid hypersonic flows.
3. Classify the viscous interactions in hypersonic flows.

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. John D. Anderson, Jr, Hypersonic and High Temperature Gas Dynamics, AIAA Series,2nd revised edition,2006,ISBN-13: 978-1563477805.
2. John. D. Anderson, Jr., Modern Compressible Flow with Historical perspective Hypersonic Series, McGraw Hill Education,3rd edition,2012,ISBN-13: 978-1259027420

Reference Books:

1. William H. Heiser and David T. Pratt, Hypersonic Air Breathing propulsion, AIAA Education Series,1994,ISBN-13: 978-1563470356
2. John T. Bertin, Hypersonic Aerothermodynamics,AIAA Inc., Washington D,1994.

For detail syllabus of all other subjects of BE As, 2017 regulation do visit As 6th Sem syllabus for 2017 Regulation.

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