Flight Dynamics detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8501), Category (PC), Contact Periods/week (5), Teaching hours/week (3), Practical Hours/week (2). The total course credits are given in combined syllabus.
For all other aero 5th sem syllabus for be 2017 regulation anna univ you can visit Aero 5th Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for flight dynamics is as follows.”
Course Objective:
- To study the performance of airplanes under various operating conditions and the static and dynamic response of aircraft for both voluntary and involuntary changes in flight conditions
Unit I
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Unit II
Manoeuvering Flight Performance
Range and endurance – Climbing and gliding flight (Maximum rate of climb and steepest angle of climb, minimum rate of sink and shallowest angle of glide) – Takeoff and landing – Turning performance (Turning rate turn radius). Bank angle and load factor – limitations on turn – V-n diagram and load factor.
Unit III
Static Longitudinal Stability
Degree of freedom of rigid bodies in space – Static and dynamic stability – Purpose of controls in airplanes -Inherently stable and marginal stable airplanes – Static, Longitudinal stability – Stick fixed stability – Basic equilibrium equation – Stability criterion – Effects of fuselage and nacelle -Influence of CG location – Power effects – Stick fixed neutral point – Stick free stability-Hinge moment coefficient – Stick free neutral points-Symmetric maneuvers – Stick force gradients – Stick force per g – Aerodynamic balancing.
Unit IV
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Unit V
Dynamic Stability
Introduction to dynamic longitudinal stability: – Modes of stability, effect of freeing the stick – Brief description of lateral and directional. dynamic stability – Spiral, divergence, Dutch roll, auto rotation and spin.
Course Outcome:
- Know about the forces and moments that are acting on an aircraft, the different types of drag, drag polar, ISA, variation of thrust, power, SFC with velocity and altitude.
- Have understanding about performance in level flight, minimum drag and power required, climbing, gliding and turning flight, v-n diagram and load factor.
- Knowledge about degrees of stability, stick fixed and stick free stability, stability criteria, effect of fuselage and CG location, stick forces, aerodynamic balancing.
- Understanding about lateral control, rolling and yawing moments, static directional stability, rudder and aileron control requirements and rudder lock.
- Understanding about dynamic longitudinal stability, stability derivatives, modes and stability criterion, lateral and directional dynamic stability.
Text Books:
- Mc Cornick. W., Aerodynamics, Aeronautics and Flight Mechanics, John Wiley, NY, 1979.
- Nelson, R.C. Flight Stability and Automatic Control, McGraw-Hill Book Co., 2004.
- Perkins, C.D., and Hage, R.E., Airplane Performance stability and Control, John Wiley and Son:, Inc, NY, 1988.
References:
- Babister, A.W., Aircraft Dynamic Stability and Response, Pergamon Press, Oxford, 1980.
- Dommasch, D.O., Sherby, S.S., and Connolly, T.F., Aeroplane Aero dynamics, Third Edition, Issac Pitman, London, 1981.
- Etkin, B., Dynamics of Flight Stability and Control, Edn. 2, John Wiley, NY, 1982.
- Mc Cornick B. W, Aerodynamics, Aeronautics and Flight Mechanics, John Wiley, NY, 1995.
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 5th Sem syllabus for 2017 Regulation.
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