Anna University Syllabus - Anna University ME Syllabus
AO7201 FLIGHT MECHANICS Syllabus | Anna University ME Aeronautical Engineering Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aeronautical engineering, Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics.
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AO7201 FLIGHT MECHANICS L T P C 3 1 0 4
OUTCOME:
Upon completion of the course, students will understand the static, dynamic longitudinal,
directional and lateral stability and control of airplane, effect of maneuvers.
UNIT I PRINCIPLES OF FLIGHT 12
Physical properties and structure of the atmosphere, International Standard Atmosphere,
Temperature, pressure and altitude relationship, Measurement of speed – True, Indicated and
Equivalent air speed, Streamlined and bluff bodies, Various Types of drag in airplanes, Drag
polar, Methods of drag reduction of airplanes.
UNIT II AIRCRAFT PERFORMANCE IN LEVEL, CLIMBING AND
GLIDING FLIGHTS 11
Straight and level flight, Thrust required and available, Power required and available, Effect of
altitude on thrust and power, Conditions for minimum drag and minimum power required, Gliding
and Climbing flight, Range and Endurance
8
UNIT III ACCELERATED FLIGHT 10
Take off and landing performance, Turning performance, horizontal and vertical turn, Pull up and
pull down, maximum turn rate, V-n diagram with FAR regulations.
UNIT IV LONGITUDINAL STABILITY AND CONTROL 15
Degrees of freedom of a system, static and dynamic stability, static longitudinal stability,
Contribution of individual components, neutral point, static margin, Hinge moment, Elevator control
effectiveness, Power effects, elevator angle to trim, elevator angle per g, maneuver point, stick
force gradient, aerodynamic balancing, Aircraft equations of motion, stability derivatives, stability
quartic, Phugoid motion
UNIT V LATERAL, DIRECTIONAL STABILITY AND CONTROL 12
Yaw and side slip, Dihedral effect, contribution of various components, lateral control, aileron
control power, strip theory, aileron reversal, weather cock stability, directional control, rudder
requirements, dorsal fin, One engine inoperative condition, Dutch roll, spiral and directional
divergence, autorotation and spin
TOTAL: 60 PERIODS
REFERENCES
1. Houghton, E.L., and Caruthers, N.B., Aerodynamics for engineering students, Edward Arnold
Publishers, 1988.
2. Perkins C.D., & Hage, R.E. Airplane performance, stability and control, Wiley Toppan, 1974.
3. Kuethe, A.M., and Chow, C.Y., Foundations of Aerodynamics, John Wiley & Sons, 1982.
4. Clancey,L.J. Aerodynamics, Pitman, 1986.
5. Babister, A.W. Aircraft stability and response, Pergamon Press, 1980.
6. Nelson, R.C. Flight Stability & Automatic Control, McGraw-Hill, 1989.
7. McCormic, B.W., Aerodynamics, Aeronautics & Flight Mechanics John Wiley,
1995.
AO7201 FLIGHT MECHANICS L T P C 3 1 0 4
OUTCOME:Upon completion of the course, students will understand the static, dynamic longitudinal,
directional and lateral stability and control of airplane, effect of maneuvers.
UNIT I PRINCIPLES OF FLIGHT 12
Physical properties and structure of the atmosphere, International Standard Atmosphere,
Temperature, pressure and altitude relationship, Measurement of speed – True, Indicated and
Equivalent air speed, Streamlined and bluff bodies, Various Types of drag in airplanes, Drag
polar, Methods of drag reduction of airplanes.
UNIT II AIRCRAFT PERFORMANCE IN LEVEL, CLIMBING AND
GLIDING FLIGHTS 11
Straight and level flight, Thrust required and available, Power required and available, Effect of
altitude on thrust and power, Conditions for minimum drag and minimum power required, Gliding
and Climbing flight, Range and Endurance
8
UNIT III ACCELERATED FLIGHT 10
Take off and landing performance, Turning performance, horizontal and vertical turn, Pull up and
pull down, maximum turn rate, V-n diagram with FAR regulations.
UNIT IV LONGITUDINAL STABILITY AND CONTROL 15
Degrees of freedom of a system, static and dynamic stability, static longitudinal stability,
Contribution of individual components, neutral point, static margin, Hinge moment, Elevator control
effectiveness, Power effects, elevator angle to trim, elevator angle per g, maneuver point, stick
force gradient, aerodynamic balancing, Aircraft equations of motion, stability derivatives, stability
quartic, Phugoid motion
UNIT V LATERAL, DIRECTIONAL STABILITY AND CONTROL 12
Yaw and side slip, Dihedral effect, contribution of various components, lateral control, aileron
control power, strip theory, aileron reversal, weather cock stability, directional control, rudder
requirements, dorsal fin, One engine inoperative condition, Dutch roll, spiral and directional
divergence, autorotation and spin
TOTAL: 60 PERIODS
REFERENCES
1. Houghton, E.L., and Caruthers, N.B., Aerodynamics for engineering students, Edward Arnold
Publishers, 1988.
2. Perkins C.D., & Hage, R.E. Airplane performance, stability and control, Wiley Toppan, 1974.
3. Kuethe, A.M., and Chow, C.Y., Foundations of Aerodynamics, John Wiley & Sons, 1982.
4. Clancey,L.J. Aerodynamics, Pitman, 1986.
5. Babister, A.W. Aircraft stability and response, Pergamon Press, 1980.
6. Nelson, R.C. Flight Stability & Automatic Control, McGraw-Hill, 1989.
7. McCormic, B.W., Aerodynamics, Aeronautics & Flight Mechanics John Wiley,
1995.
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