Performance I Flashcards
What is the key element for determining an aircraft’s performance?
The drag polar.
CD stands for (note the capital D)?
The drag coefficient for the entire aircraft.
C_D_0 stands for?
The parasite drag coefficient for the aircraft.
The Oswald efficiency factor is represented using the symbol ___.
e
For basic performance, lift is considered to be _______.
Perpendicular to the flight path direction and equal and opposite to the weight.
For basic performance, drag is considered to be _____ to the flight path direction.
Parallel
True or False
For an aircraft in flight, the thrust is often inclined with respect to the flight path although the angle is usually small.
True
The angle between the horizontal plane and the flight path is given the symbol ____.
theta
True or False
The flight path is drawn in a straight line, however, the AC is generally traveling in a curved path (especially when viewed from a distance).
True
In the most basic sense, all flight is ______ as opposed to straight.
Curvilinear
The case where the acceleration of the aircraft is equal to zero is referred to as _________.
Static performance.
For completely level flight, the angle between the horizontal and the flight path is _______.
Zero
True or False
In steady level flight with no acceleration or disturbances, T = D and L = W.
True
Thrust required varies proportionally with _______ and inversely with ______.
The drag coefficient times the weight
The lift coefficient
T = (CD*W)/CL = W/(CL/CD)
Thrust required varies inversely with the _____ ratio.
Lift to Drag
The thrust required is directly proportional to the ____ ratio.
Drag to lift (D/L)
Note: T = 1/(L/D) = D/L
Since Thrust required varies ____ with the lift to drag ratio, the minimum thrust required will occur when ______.
Inversely
The aircraft is flying at a velocity where the L/D ratio is at a maximum