Level of Contribution |
|||||
---|---|---|---|---|---|
0 | 1 | 2 | 3 | 4 | 5 |
Compulsory Course Units |
||||||||
---|---|---|---|---|---|---|---|---|
Name of the Course Unit | 1 | 2 | 3 | 4 | 5 | 6 | T | % |
INTRODUCTION TO THESIS AND SEMINAR | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
INTRODUCTION TO THESIS AND SEMINAR | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
TERM PROJECT | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
TERM PROJECT | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
SCIENTIFIC RESEARCH TECHNIQUES AND PUBLICATION ETHICS | 3 | 2 | 3 | 2 | 2 | 2 | 14 | 8,14 |
SCIENTIFIC RESEARCH TECHNIQUES AND PUBLICATION ETHICS | 3 | 2 | 3 | 2 | 2 | 2 | 14 | 8,14 |
THESIS-I | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
THESIS-I | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
THESIS-II | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
THESIS-II | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
TOTAL | 6 | 4 | 6 | 4 | 4 | 4 | 28 | 16,28 |
Course-Programme Outcome Relationship |
||||||||
---|---|---|---|---|---|---|---|---|
Name of the Course Unit | 1 | 2 | 3 | 4 | 5 | 6 | T | % |
DC-DC CONVERTERS AND ANALYSIS | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
MODERN DIGITAL COMMUNICATION | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
ADVANCED PRODUCTION TECHNIQUES | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
CONVECTION HEAT TRANSFER | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
COMPUTATIONAL FLUID DYNAMICS | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
COMPOSITE MATERIALS IN AIRCRAFT | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
AIRCRAFT DYNAMICS | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
ADDITIVE MANUFACTURING AND 3D PRINTER TECHNOLOGIES | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
AIRCRAFT ICING | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
FINITE ELEMENT ANALYSIS OF STRUCTURES | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
AEROSPACE MATERIALS AND PRODUCTION METHODS | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
APPLIED NONLINEAR CONTROL | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
ADVANCED PROPULSION SYSTEMS | 5 | 5 | 5 | 5 | 5 | 5 | 30 | 23,81 |
ADVANCED CONTROL SYSTEMS | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
HEAT TRANSFER BY CONVECTION | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
UNMANNED AERIAL VEHICLE DESIGN | 5 | 5 | 5 | 3 | 3 | 4 | 25 | 19,84 |
AIRFOIL ANALYSIS AND DESIGN | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
VISCOUS FLOW | 5 | 5 | 5 | 4 | 4 | 5 | 28 | 22,22 |
NUMERICAL METHODS IN ENGINEERING | 4 | 3 | 4 | 4 | 3 | 2 | 20 | 15,87 |
ENGINEERING MATHEMATICS | 5 | 4 | 4 | 3 | 3 | 5 | 24 | 19,05 |
INTERNAL COMBUSTION ENGINE | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
TOTAL | 24 | 22 | 23 | 19 | 18 | 21 | 127 | 100,79 |