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:
After studying the course the students will be able to
Conduct of Practical Examination:
1 . All laboratory experiments 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 :