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問題一覧
1
Where Laminar smooth flowing turns into Turbulent flow, is where the Reynolds Number reaches critical value
Transition Point
2
Air is the fluid through which airplanes move
Drag
3
Contributes to Aerodynamic Drag
Skin Friction Drag
4
is comprised of all the forces that work to slow an aircraft’s movement.
Parasite Drag
5
this type of stall are practiced to simulate normal approach-to-landing conditions and configurations
Arrival Stall
6
Assumed to involve no friction, thermal conduction, or diffusion
Inviscid Flow
7
The relationship between the drag coefficient and the lift coefficient.
Drag Polar
8
Are smooth and regular and the fluid elements smoothly along the streamlines
Laminar Flow
9
More severe than un-accelerated stalls and are often unexpected
Accelerated Stall
10
A condition in aerodynamics and aviation wherein the AOA increases beyond a certain point such that lift begins to decrease
Stall
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Breaks up and a fluid elements move in a random, irregular torturous fashion
Turbulent Flow
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Causes shear stress at the surface
Air Friction
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simulates a base to final skidding turn, where pilots may apply aileron in one direction rudder in the direction.
Cross Controlled Stall
14
As the air and vortices roll off the back of your wing, they angle down
Downwash
15
occurs when you pull the aircraft nose up too high while maintaining full power.
power on stall
16
is the portion of parasite drag generated by the aircraft due to its shape and airflow around it.
Form Drag
17
this type of stall are practiced to simulate take-off and climb-out conditions and configurations
Departure Stall
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Measure of ratio if inertial forces to viscous forces
Reynold’s Number
19
is the aerodynamic resistance due to the contact of moving air with the surface of an aircraft.
Skin Friction Drag
20
comes from the intersection of airstreams that creates eddy currents, turbulence, or restricts smooth airflow.
Interference Drag
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Pressure drag due to separation
Flow Separation
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The second basic type of drag
Induced Drag
23
Sticky or adhesive characteristic of a fluid.
Viscosity
24
occurs when an aircraft is in a landing configuration, usually with the landing gear down and reduced power.
power off stall
25
The region of viscous flow which has been retarded owing to friction at the surface
Boundary Layer