Content :
UNIT-1
CRUISING FLIGHT PERFORMANCE
- International standard atmosphere
- Four force of flight
- Equations of motion
- Different types of drag
- 1. The shape of the object and frontal area
- 2. The square of the velocity
- 3. The density of the fluid
- Drag polar
- Thrust required (drag)
- Power required
- Graphical approach
- Analytical approach
- Power available and maximum velocity
- Propeller driven aircraft
- Mandeuvering flight performance
- Range
- Specific fuel consumption for a propeller
- Range for propeller-driven airplanes
- Endurance
- Endurance for jet propelled airplanes
- Rate of climb
- Graphical approach
- Maximum climb angle
- Maximum rate of climb
- Gliding (unpowered) flight
- Level turn
- Minimum turn radius
- Maximum turn rate
- Pull-up and pull-down maneuvrs
- Limiting case for large load factors
- v-n diagram
STATIC LONGITUDINAL STABILITY
- Derivation of rigid body equation of motion
- Power effects
- Stick-fixed neutral point
- Stick forces
- Stick-force gradients
- Stick –free neutral point
- Static margin
- Aerodynamic balancing
- Types
- 1. Control horns
- 2. Fries ailerons
- 3. Over hang balance
- 4. Internal balance
- 5. Tabs
- 6. Mass balancing
- Longitudinal static stability
- Equation for static stability
- Wing-contribution
- Tail contribution
- Fuselage contribution
- Pitching
- Moment curves
- Neutral point
LATERAL AND DIRECTIONAL STABILITY
- Lateral (rolling) stability
- Wing dihedral
- Coupling between rolling and yowing moments
- Static-directional stability
- Adverse yaw effects
- Rudder requirements
- 1. Slipstream rotation
- 2. Cross-winds during take-off and landing
- 3. Spinning
- 4. Anti-symmetric power
- Aileron reversal
- Rudder lock
- One-engine in operative condition
DYNAMIC STABILITY
- Dynamic stability
- Longitudinal dynamic stability
- Types
- 1. The short period pitching oscillation
- 2. The phugoid
- Dynamic directional stability
- Lateral dynamic stability
- 1. Directional divergence
- 2. Spiral divergence
- 3. Dutch roll
- Auto rotation
- The spin