Wake Turbulence and Wind Shear Flashcards
As you should recall from basic aerodynamics, higher AOA means greater induced drag. Based on that knowledge and what you just learned about the relationship between induced drag and vortex intensity, which flap configuration do you think will cause increased wake turbulence strength?
Flaps up
What are factors which primarily affect the strength of vortices?
Weight, speed, and wing configuration
An aircraft flying in which position would experience an induced roll to the left?
Behind the right wingtip
True or false: Pilots of small aircraft should avoid operating within 2 rotor diameters of a hovering helicopter due to downwash hazards. However, since a helicopter does not generate wake turbulence, normal spacing rules do not apply.
False
When taking off behind a heavy aircraft (over 255,000 pounds) established spacing requirements are ______ minute(s) minimum. This spacing is also encouraged behind large aircraft (41,000 to 255,000 pounds).
2
Minimum landing spacing requirement is ______ minute(s) behind a heavy aircraft (over 255,000 pounds).
3
Wind shear is defined as a sudden change in wind ______ over a short distance in the atmosphere.
Speed and/or direction
A microburst will most likely be encountered in areas of heavy ______.
Rain
When viewed from behind the generating aircraft, wingtip vortices rotate ______ from the right wing and ______ from the left wing.
Counterclockwise; clockwise
Wake turbulence is generated ______.
By any aircraft whenever it is producing lift
When taking off behind a heavy aircraft in the T-6A, you should allow for a minimum spacing of ______ minute(s).
2
When taking off behind a heavy aircraft that has just landed, what should you do to minimize the effects of its wake turbulence?
Plan to lift off after its nose gear touchdown point
Key hazards created by wake turbulence are ______ and ______.
Induced roll; induced flow field
True or false: The wake turbulence generated by a heavy aircraft taking off from a parallel or intersecting runway is not a factor for aircraft operating on another runway.
False
How will a wind shear that decreases your headwind component by 20 knots affect your aircraft?
Indicated airspeed will decrease 20 knots thereby decreasing lift.