Heat and Mass Transfer detailed Syllabus for Aeronautical Engineering (AERO), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information, visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.
For all the other VTU AERO 7th Sem Syllabus for BE 2018 Scheme, visit Aeronautical Engineering 7th Sem 2018 Scheme.
For all the (Professional Elective-2) subjects refer to Professional Elective-2 Scheme. The detail syllabus for heat and mass transfer is as follows.
Course Objectives:
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Module 1
Fundamentals: Different modes of heat transfer and mass and momentum transfer, elements of mass diffusion and boundary layer theory. Mass transfer definition and terms used in mass transfer analysis, Fick’s First law of diffusion.
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
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Module 4
Radiation &Heat Exchangers Design: Radiation: Introduction to physical mechanism-Radiation properties-Radiation shape factors-Heat exchange between non-black bodies-Radiation shields Heat Exchangers: Classification of heat exchangers; overall heat transfer coefficient, fouling and fouling factor; LMTD, Effectiveness-NTU methods of analysis of heat exchangers. Numerical problems.
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. Heat transfer problems in turbine and nozzle blades.
Course Outcomes:
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Question paper pattern:
- The question paper will have ten full questions carrying equal marks.
- Each full question will be for 20 marks.
- There will be two full questions (with a maximum of four sub- questions) from each module.
- Each full question will have sub- question covering all the topics under a module.
- The students will have to answer five full questions, selecting one full question from each module.
Text Books:
- Heat transfer-A basic approach Ozisik Tata McGraw Hill 2002
- Heat Transfer Holman, J.P McGraw Hill Book Co., Inc., New York 8th edition,1996
Reference Books:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
For the detail Syllabus of all other subjects of BE (AERO) 7th Sem, visit Aeronautical Engineering 7th Sem Subjects.
For all (CBSE & Non-CBSC) BE/B.Tech results, visit VTU BE/B.Tech all semester results.