Unit 1
Hours: 8
Introduction (aero-elastic phenomena and design requirements), Introduction to missiles & systems, Design process.
| Course Name | Aerospace System Configuration, Design and Simulation |
| Course Code | 25DT611 |
| Program | M.Tech. in Defence Technology |
| Semester | 2 |
| Credits | 4 |
| Campus | Coimbatore |
Hours: 8
Introduction (aero-elastic phenomena and design requirements), Introduction to missiles & systems, Design process.
Hours: 8
Structural requirement, Structural and aerodynamic stiffness, Static aero-elasticity: torsional divergence, Structural vibration and modal analysis.
Hours: 9
Aerodynamic loads on an oscillating lifting surface, Characteristics of flutter and important design parameters, Methods for aero-elastic analysis, Computational fluid dynamics, advances in aero dynamics (Hypersonic Flows and Aerodynamic Heating).
Hours: 8
Aircraft performance (cruising, climb, descent, takeoff, landing, maneuver, flight path).
Hours: 9
System’s stability & control, aerodynamics control, Introduction to dynamic stability, first and second order responses, Equations of motion and modal characteristics.
Hours: 8
Introduction to air to air, ground to air, air to ground weapon systems, UAV mounted GW and UCAVs.
Total: 50
Course Objectives
The main objective of the course is to provide knowledge to the students about the process & techniques of aerospace system design, meeting the specified design requirements. They will also learn about carrying structural and aerodynamic analysis, performance evaluation of aircraft and stability analysis.
Course Outcomes:
At the end of the course the student should be able to:
References / Suggested Books:
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