Modelling & Analysis Lab 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 do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.
For all other VTU AERO 7th Sem Syllabus for BE 2018 Scheme, do visit VTU AERO 7th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for modelling & analysis lab is as follows.
Course Objectives:
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.
.
List of Experiments:
- Modeling of Symmetrical/Cambered Aerofoil Geometry , and Generation of Body Fitting Adaptive Mesh.
- Modeling of 2-D Incompressible and Invisicd Flow over Symmetrical/Cambered Aerofoil, and Plotting of Pressure distribution and Velocity vectors for Subsonic/Supersonic Mach numbers.
- Modeling of 2-D Compressible and Viscid Flow over Symmetrical/Cambered Aerofoil, and Plotting of Pressure distribution and Velocity vectors for Subsonic Mach numbers.
- Isentropic Flow Analysis in a 2-D Subsonic Diffuser and a Subsonic Nozzle.
- Isentropic Flow Analysis in a 2-D Supersonic Diffuser and a Supersonic Nozzle.
- Geometric Modeling and Mesh Generation of a 2-D Convergent-Divergent Nozzle and Analyses of flow for Adiabatic Conditions (Fanno Flow).
- Geometric Modeling and Mesh Generation of a 2-D Pipe and Modeling of Steady/Unsteady Heat Convection and Conduction (Rayleigh Flow).
- Structural Modeling of Sandwich Beam of Rectangular Cross-section and Analyses for Stress for
- Stnictural Modeling and Stress Analysis of a Torsion Box of a Wing.
- Structural Modeling and Stress Analysis of a Fuselage Frame.
- Structural Modeling and Stress Analysis of a Tapered I-Section Spar.
- Determine the Natural frequency and Mode shapes of a Cantilever beam under UDL.
- A Plate fixed at one end has a hole in centre and has varying thickness, Determine stresses developed due to applied static loads in vertical direction.
- A Tapered Plate fixed at one end has a hole in centre and has varying thickness, determine stresses developed due to applied static loads in vertical direction.
Course Outcomes:
At the end of the course the student will be able to:
- Draw the geometric models of symmetric, cambered aerofoil, nozzle, wing and other structures.
- Apply different types of meshing.
- Perform the flow and stress analysis.
Conduct of Practical Examinations:
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 detail Syllabus of all other subjects of BE 7th Sem Aeronautical Engineering, visit (AERO) 7th Sem Syllabus Subjects.
For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.