Flight Dynamics (AE2301) Scanned Lecture Notes (All Units) - Subhamathi Edition

  • 8Jan
  • 2015
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    Anna University , Chennai

    Department of B.E-Aeronautical Engg

    5 Semester

    AE2301 Flight Dynamics 

    (Regulation 2008 ) 

    Attachment: Click here

    Content:
    UNIT-1
    CRUISING FLIGHT PERFORMANCE
    Geometric altitude
    Performance
    Atmospheric gases
    Forces and moments acting on a flight vehicle
    Types of drag
    1. Pressure drag
    2. Skin friction drag
    3. Parasite drag
    4. Induced drag
    5. Wave drag
    Drag polar
    Minimum drag condition
    Problem

    UNIT-2
    MANOEUVERING FLIGHT PERFORMANCE
    Range for propeller driven airplane
    Range for jet propelled airplane
    Endurance
    Endurance for propeller driven airplane
    Maximum climb angle
    Maximum rate of climb
    Level turn
    Constraints on load factor
    Expression for maximum load factor
    Structural limitation
    1. Limit load factor
    2. Ultimate load factor
    Take off performance
    Loading performance
    Landing distance
    Gliding flight


    UNIT-3
    STATIC LONGITUDINAL STABILITY
    Static stability
    Dynamic stability
    Statically unstable
    Neutrally stable
    Requirements of control system
    Criteria for longitudinal stability
    Contribution of wing to longitudinal static stability
    Contribution of tail to MCG
    Contribution of tail
    Total pitching moments about CG
    Static longitudinal control
    1. Stick fixed condition
    2. Stick free condition
    Elevator hinge moments
    Aerodynamic balancing
    Set-back hinge
    Horn balance
    Sealed nose balance
    Geared tab balance
    Power effects on static and longitudinal stability

    UNIT-4
    LATERAL AND DIRECTIONAL STABILITY
    Lateral stability
    Adverse aileron yaw
    Rudder requirements
    Asymmetric power
    Spin recovery
    Condition for static lateral stability
    Aileron effectiveness
    Rudder lock
    Dorsal yin

    UNIT-5
    DYNAMIC STABILITY
    Dynamic effects
    Directional stability
    Spiral divergence
    Dutch roll
    Autorotation
    Spin
    Flat spin
    Angle of incidence
    Routh’s descriminent
    Directional stability
    Aileron reversal
    Phugoid
    Side slip angle
    Lateral stability
    Components contributing for lateral stability
    Vertical tail
    Fuselage
    Dorsal fin
    Vertical fin
    Side slip
    Contribution of components to directional stability
    1. Swept back wing
    2. Dihedral wing
    Contribution of fuselage
    Dorsal fin and vertical fin
    Lateral static stability
    Plan of symmentry
    Effects of dihedral
    Advantages 
    Disadvantages

    Attachment: Click here