Aerodynamics Flashcards
(27 cards)
What is the relationship of lift, drag, thrust and weight when the airplane is in straight-and-level unaccelerated flight?
Lift equals weight, and thrust equals drag
Airplanes climb because of
Excess thrust
The minimum forward speed of an airplane is called the _______ speed.
stall
You can determine the proper climb altitude for your airplane by referring to the
airspeed indicator
The chord line is used to represent
The general shape of the wing
Relative wind results from the motion of the
airplane through the air
relative wind is called relative because it
results from the motion of the airplane
Relative wind is ______ and _____ to the airplanes motion
opposite to, equal
Relative wind is _____ which way the airplanes nose is pointed
independent of
An important principle to understand when dealing with angle of attack is that the nose (therefore the wing) can be pointed on an incline thats _____ the actual climb path
different from
Bernoulli figured out that the faster the air flows over a surface, the ________ pressure it exerts on that surface.
less
Air flowing faster over a curved surface causes a slight _______ in pressure on that surface
decrease
Raising the nose slightly increases the angle of attack which forces the air to undergo an additional________ greater than that which the _________ of the airfoil can produce
curve, engineered shape
An increased angle of attack permits the airplane to produce the necessary lift for flight at a ___________ airspeed
slower
When the weight of an airplane is increased, the airplane stalls at __________ indicated speed
higher
the critical angle of attack at which the wing stalls _______
Never changes, regardless of airplane weight
in what flight condition must an aircraft be placed in order to spin
stalled
during a spin to the left, which wings is are stalled
both wings are stalled
wings are designed to deflect air _________ while offering very little _________ resistance.
vertically, horizontal
As airspeed doubles, parasite drag ________
quadruples
as the airplane speeds up, induced drag ________ while parasite drag _____
decreases, increases
wingtip vortex action increases with an increase in
angle of attack
ground effect results from a/an _________ in induced drag
decrease
as the airplane becomes airborne and flies out of ground effect, the wings downwash ______
increases