Advanced Computational Aerodynamics detailed syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUHs official website and presented for the students of B.Tech Aeronautical Engineering branch affiliated to JNTUH course structure. For Course Code, Course Titles, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The syllabus PDF files can also be downloaded from the universities official website.
For all the other AERO 4th Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH scheme, visit Aeronautical Engineering 4th Year 1st Sem R18 Scheme.
For all the (Professional Elective-3) subjects refer to Professional Elective-3 Scheme. The detail syllabus for advanced computational aerodynamics is as follows.
Pre-Requisites:
CFD
Course Objective:
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Course Outcome:
- Different techniques to solve the complex fluid dynamics problem numerically
Unit – I
Numerical Solutions: Euler equations: Flux approach, Lax-Wendroff method, basic principles of upwind schemes, flux vector splitting, Steger Warming flux vector splitting, Van Leer flux vector splitting, Upwind reconstruction, evolution, Godunov�s first order upwind method, Roe�s first order upwind method.
Unit – II
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Unit – III
Boundary Conditions: Boundary Layer Equations: Setting up the boundary layer equations, flat plate boundary layer solution, boundary layer transformations, explicit and implicit discretization, solution of the implicit difference equations, integration of the continuity equation, boundary layer edge and wall shear stress, Keller-box scheme. Concept of dummy cells, solid wall inviscid flow, viscous flow, farfield concept of characteristic variables, modifications for lifting bodies inlet outlet boundary, injection boundary, symmetry plane, coordinate cut, periodic boundaries, interface between grid blocks, flow gradients at boundaries of unstructured grids.
Unit – IV
Method of Characteristics: Philosophy of method of characteristics, determination of characteristic lines, two dimensional irrotational flow, determination of compatibility equations, unit processes, supersonic nozzle design by the method of characteristics, supersonic wind tunnel nozzle, minimum length nozzles, domain of dependence and range of influence.
Unit – V
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Text Books:
- Tannehill John C, Anderson Dale A, Pletcher Richard H, Computational Fluid Mechanics and Heat Transferll, Taylor and Francis, 2nd Edition, 1997.
- Chung T G, Computational Fluid Dynamics!, Cambridge University Press, 2nd Edition, 2010.
- Katz Joseph and Plotkin Allen, Low-Speed Aerodynamicsl, Cambridge University Press, 2nd Edition, 2006.
Reference Books:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
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For detail syllabus of all other subjects of B.Tech Aeronautical Engineering 4th Year 1st Sem , visit AERO 4th Year 1st Sem syllabus subjects.
For B.Tech Aeronautical Engineering (AERO) 4th Year results, visit JNTUH B.Tech Aeronautical Engineering semester results direct link.