Heat and Mass Transfer detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AE53), 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 5th sem syllabus for be 2017 scheme vtu you can visit Aero 5th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for heat and mass transfer is as follows.
Course Objectives:
This course will enable students to
- Understand the different modes of heat transfer.
- Understand the free convection and forced convection.
- Acquire the knowledge of heat transfer problems in combustion chambers.
Module 1
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Module 2
Conduction: Derivation of general three dimensional conduction equation in Cartesian coordinate, special cases, discussion on 3-D conduction in cylindrical and spherical coordinate systems. Effect of variation of thermal conductivity on heat transfer in solids – Heat transfer problems in infinite and semi-infinite solids – Extended surfaces. One dimensional transient heat conduction: Systems with negligible internal resistance, Significance of Biot and Fourier Numbers, Chart solutions of transient conduction systems.
Module 3
Convection: Concepts of Continuity, Momentum and Energy Equations. Dimensional analysis-Buckingham’s Pi Theorem -Application for developing non-dimensional correlation for convective heat transfer
Free Convection: Development of Hydrodynamic and thermal boundary layer along a vertical plate , Use of empirical relations for Vertical plates and pipes.
Forced Convection: External Flows, Concepts of hydrodynamic and thermal boundary layer and use of empirical correlations for Flat plates and Cylinders. Internal Flows, Concepts about Hydrodynamic and Thermal Entry Lengths, use of empirical correlations for Horizontal Pipe Flow and annulus flow.
Module 4
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Module 5
Heat and Mass Transfer Problems in Aerospace Engineering: Heat transfer problems in gas turbine combustion chambers – Rocket thrust chambers – Aerodynamic heating -Ablative heat transfer. Mass Transfer: Introduction, Ficks law, Species conservation equation, Introduction to convective and diffusive mass transfer.
Course Outcomes:
After studying this course, students will be able to:
- Describe the fundamental of heat and mass transfer.
- Familiarize the student in the area of conduction, convection and radiation.
- Analyze the problems due to heat transfer in several areas.
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 2full 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:
- Ozisik, Heat transfer-A basic approach, Tata McGraw Hill 2002
- Holman, J.P., ” Heat Transfer “, McGraw Hill Book Co., Inc., New York, 8th edition., 1996, ISBN-13: 978-0071143202
Reference Books:
- Sachdeva, S.C., ” Fundamentals of Engineering Heat and Mass Transfer , Wiley Eastern Ltd., New Delhi, 1981.
- Sutton, G.P., Rocket Propulsion Elements “, John Wiley and Sons, 5th Edn.1986.
- Mathur, M.and Sharma, R.P., ” Gas Turbine and Jet and Rocket Propulsion , Standard Publishers, New Delhi 1988.
- P.K. Nag, Heat transfer, Tata McGraw Hill 2002
- Yunus A- Cengel , Heat transfer, a practical approach, Tata McGraw Hill , 3rd edition, 2007.
For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 5th Sem syllabus for 2017 scheme.
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