Tutorials Flashcards
Notation for coefficient of lift of a) wing b) aerofoil
a) CL
b)Cl
Notation for lift and drag of a) wing and b) horizontal tail
a) Lw, Dw
b)Lt, Dt
Are pitching moment coefficient notation Cm and CM different?
No, they are used interchangeably
What does ε represent
the downwash angle behind the wing, i.e. the angle by which the airflow is deflected behind a wing due to the effects of vortices
What is the angle of incidence, i?
The angle between the chord line of the wing where the wing is mounted to the fuselage, and a reference axis along the fuselage
What is xac,w?
The wing aerodynamic centre location from the wing leading edge
What is xcg?
The location of the centre of gravity from the leading edge of the aircraft
How are wing reference area, wing span, and mean aerodynamic chord denoted?
S or Sw
b
Cbar
What symbols correspond to a) ailerons, b) elevators, and c) rudders
a) ξ (xi)
b) η (eta)
c) ζ (zeta)
What are the sign conventions for control surface movement?
1) positive aileron=> port wing down
2) Positive elevator=>nose down
3)positive rudder=>nose to port
Which side is port and which is starboard
port=left
starboard=right
What rotation does a) elevator, b) ailerons, c) rudder provide
a) pitch
b) roll
c) yaw
Where is the body fixed coordinate system centred?
At the centre of gravity of the aircraft
Is centre of gravity fixed?
No it moves as payload changes, fuel is consumed and as other factors changes
The simplest trim condition is straight and level flight, what does this mean?
The forces are balanced and the moments about the CoG sum to zero. Accelerations and angular accelerations are all zero.
Which surface most strongly influences longitudinal trim
The elevator
What is the best way to begin discussing airplane trim and stability?
With quasi-static analysis:
pitching moment about CoG is first considered, followed by the changes in pitching moment generated when the vehicle changes pitch
What does quasi-static mean
Unsteady aerodynamic and inertial effects are neglected