BAE701

Flight Mechanics

L-T-P3-0-0 Credits3 Session2025-26 TypeTheory
Appears in 1 semester

B.Tech Aeronautical Engineering · Sem 7 (Core)

Syllabus

5 units
Unit1

Unit 1: Atmospheric Properties and Flight Fundamentals

8 Hours Standard atmosphere; types of altitude including geopotential, geometric, pressure, temperature, and density altitude; forces and moments acting on a flight vehicle; equations of motion of a rigid flight vehicle; types of drag and drag polar; types of airspeeds and instruments including airspeed indicator, altimeter, rate-of-climb indicator, and Mach meter; variation of thrust and power with velocity and altitude for air-breathing engines.

Unit2

Unit 2: Cruising and Maneuvering Flight Performance

8 Hours Performance of an airplane in level flight; power available and power required curves; maximum speed in level flight; conditions for minimum drag and minimum power required; range and endurance of aircraft; climbing and gliding flight including maximum rate of climb and steepest angle of climb, minimum rate of sink and shallowest angle of glide; turning rate and turn radius, bank rate and bank angle; load factor and its limitations on turns; V-n diagram and gust envelope; take-off and landing performance.

Unit3

Unit 3: Static Longitudinal Stability

8 Hours Static stability fundamentals; purpose of controls in airplanes; static longitudinal stability including stick-fixed and stick-free concepts, basic equilibrium equation, stability criterion, effects of fuselage and tail, influence of center of gravity (CG) location, power effects, neutral points, and stick force gradients.

Unit4

Unit 4: Static Lateral and Directional Stability

8 Hours Dihedral effect; lateral control; coupling between rolling and yawing moments; roll stability and control including adverse yaw effects and aileron reversal; static directional stability and control including weathercock effect, rudder requirements, rudder lock, aerodynamic balancing; pedal-fixed and pedal-free stability; roll control reversal.

Unit5

Unit 5: Dynamic Stability

8 Hours Degrees of freedom of rigid bodies in space; dynamic longitudinal and lateral-directional stability; Euler angles; velocities in three directions; decoupling of longitudinal and lateral-directional dynamics; dynamic stability modes including phugoid, short-period, spiral divergence, Dutch roll, autorotation, and spin; effects of freeing the stick; approximation of modes and factors affecting time period and damping.

Course Outcomes (COs)5 outcomes

After completion of the course student will be able to:

  1. CO1Understand atmospheric properties and fundamental flight principles.K2
  2. CO2Analyze cruising and maneuvering flight performance parameters.K4
  3. CO3Explain static longitudinal, lateral, and directional stability concepts.K2
  4. CO4Describe dynamic stability modes and their effects on aircraft behavior.K2
  5. CO5Apply stability and performance theories to evaluate aircraft flight characteristics.K3

Textbook

  1. and References:
  2. Anderson, J.D., Introduction to Flight, Tata McGraw-Hill.
  3. Perkins, C.D., and Hage, R.E., Airplane Performance, Stability and Control, John Wiley & Sons.
  4. Nelson, R.C., Flight Stability and Automatic Control, McGraw-Hill Book Company.
  5. McCormick, B.W., Aerodynamics, Aeronautics and Flight Mechanics, John Wiley & Sons.
  6. Babister, A.W., Aircraft Dynamic Stability and Response, Pergamon Press, Oxford.

Official AKTU syllabus

This subject is on page 4 of the original AKTU PDF.

Official AKTU syllabus PDF ↗