Flight Simulation Lab Aero 7th Sem Syllabus for VTU BE 2017 Scheme

Flight Simulation Lab detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AEL76), 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 flight simulation lab is as follows.

Course Objectives:

This course will enable students to

• Understand the root locus and bode plot.
• Understand the spring mass damper system and the servo mechanism system with feedback.
• Acquire the knowledge to use computational tools to model aeronautical vehicle dynamics.
1. Draw Pole-Zero map of dynamic system model with plot customization option
2. Plot root locus with variables in transfer function through MATLAB
3. Plot root locus for a dynamic system though MATLAB
4. Draw Bode plot from a transfer function phase margins in MATLAB and explain the gain and
5. Simulate a spring- mass- damper system with and without a forcing function though SIMULINK
6. Simulate a simple servo-mechanism motion with feedback- in the time domain, and in ‘s’ domain
7. Simulate a bomb drop from an aircraft on a moving tank in pure pursuit motion
8. Develop a straight and level flight simulation program using MATLAB
9. Simulate aircraft Take-off and Landing with trajectory tracing
10. Simulate stall of aircraft and show the effect of variation in static margin on stalling characteristics
11. Simulate aircraft longitudinal motion and demonstrate the effect of static margin variation for a pulse input in pitch that is intended to bleed the airspeed.
12. Simulate aircraft longitudinal motion and demonstrate the effect of static margin variation for a doublet input in pitch
13. Given a Quartic characteristic equation, determine two quadratics that shall result in poles of short-period oscillations and poles of Phugoid. Vary the coefficients of polynomial to study the movement of poles.
14. Given a Quartic characteristics equitation, determine Poles and Time constants for Roll mode, Spiral motion, and Dutch roll. Vary the coefficients of polynomial to study the movement of poles.

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.
• Design / development of solutions (partly) Interpretation of data.

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

Dont forget to download iStudy for latest syllabus and results, class timetable and more.