Modeling and Analysis Lab Aero 7th Sem Syllabus for VTU BE 2017 Scheme

Modeling and Analysis Lab detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AEL77), 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 7th sem syllabus for be 2017 scheme vtu you can visit Aero 7th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for modeling and analysis lab is as follows.

Course Objectives:

This course will enable students to

• Understand the procedure to draw the geometric models of symmetric, cambered aerofoil, nozzle, wing and other structures.
• Acquire the knowledge of types of meshing.
• Understand the basics of flow and stress analysis.
1. Modeling of Symmetrical/Cambered Aerofoil Geometry , and Generation of Body Fitting Adaptive Mesh.
2. 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.
3. Modeling of 2-D Compressible and Viscid Flow over Symmetrical/Cambered Aerofoil, and Plotting of Pressure distribution and Velocity vectors for Subsonic Mach numbers.
4. Isentropic Flow Analysis in a 2-D Subsonic Diffuser and a Subsonic Nozzle.
5. Isentropic Flow Analysis in a 2-D Supersonic Diffuser and a Supersonic Nozzle.
6. Geometric Modeling and Mesh Generation of a 2-D Convergent-Divergent Nozzle and Analyses of flow for Adiabatic Conditions (Fanno Flow).
7. Geometric Modeling and Mesh Generation of a 2-D Pipe and Modeling of Steady/Unsteady Heat Convection and Conduction (Rayleigh Flow).
8. Structural Modeling of Sandwich Beam of Rectangular Cross-section and Analyses for Stress for Unsymmetrical bending case.
9. Structural Modeling and Stress Analysis of a Torsion Box of a Wing.
10. Structural Modeling and Stress Analysis of a Fuselage Frame.
11. Structural Modeling and Stress Analysis of a Tapered I-Section Spar.
12. Determine the Natural frequency and Mode shapes of a Cantilever beam under UDL.
13. 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.
14. 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:

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Conduct of Practical Examinations:

1. All lab practicals are to be included for practical examination.
2. Students are allowed to pick one experiment from the lot.
3. Strictly follow the instructions as printed on the cover page of answer script for breakup of marks.
4. Change of experiment is allowed only once and 15% Marks allotted to the procedure part to be made zero.

Graduate Attributes (as per NBA):

• Engineering Knowledge.
• Problem Analysis.
• Team work
• Communication

For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 7th Sem syllabus for 2017 scheme.

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