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I want the syllabus of Flight Dynamics of BE Aeronautical Engineering of Anna University so will you please provide me?

[Vishal Kotkar]

I am providing you the syllabus of Flight Dynamics of BE Aeronautical Engineering of Anna University

Anna University BE Aeronautical Engineering Flight Dynamics syllabus

AE2301 FLIGHT DYNAMICS L T P C

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 CRUISING FLIGHT PERFORMANCE 10

International Standard Atmosphere - Forces and moments acting on a flight vehicle -
Equation of motion of a rigid flight vehicle - Different types of drag –estimation of parasite
drag co-efficient by proper area method- Drag polar of vehicles from low speed to high
speeds - Variation of thrust, power with velocity and altitudes for air breathing engines .
Performance of airplane in level flight - Power available and power required curves.
Maximum speed in level flight - Conditions for minimum drag and power required

UNIT II MANOEUVERING FLIGHT PERFORMANCE 11

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) -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 10

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 LATERAL AND DIRECTIONAL STABILITY 8

Dihedral effect - Lateral control - Coupling between rolling and yawing moments - Adverse
yaw effects - Aileron reversal - Static directional stability - Weather cocking effect - Rudder
requirements - One engine inoperative condition - Rudder lock.

UNIT V DYNAMIC STABILITY 6

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.

TOTAL: 45 PERIODS

TEXT BOOKS

1. Perkins, C.D., and Hage, R.E., “Airplane Performance stability and Control”, John
Wiley & Son:, Inc, NY, 1988.

2. Nelson, R.C. “Flight Stability and Automatic Control”, McGraw-Hill Book Co., 2004.

3. Mc Cornick. W., “Aerodynamics, Aeronautics and Flight Mechanics”, John Wiley, NY,1979.

REFERENCES

1. Etkin, B., “Dynamics of Flight Stability and Control”, Edn. 2, John Wiley, NY, 1982.

2. Babister, A.W., “Aircraft Dynamic Stability and Response”, Pergamon Press, Oxford,1980.

3. Dommasch, D.O., Sherby, S.S., and Connolly, T.F., “Aeroplane Aero dynamics”, Third Edition, Issac Pitman, London, 1981.

4. Mc Cornick B. W, “Aerodynamics, Aeronautics and Flight Mechanics”, John Wiley, NY,1995.

Contact-

Anna University
Kotturpuram
Chennai, Tamil Nadu