causes of wake turbulence (copy)

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Last updated 12:50 PM on 4/22/26
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38 Terms

1
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Convective currents, mechanical disturbances, ____, and ___ are the four main causes of turbulence.

wind shear, wake turbulence

2
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What are the 5 causes of wake turbulence?

  • Wing-tip vortices

  • Rotor-tip vortices

  • Jet engine thrust stream (or Jet blast)

  • Rotor downwash

  • Prop wash

3
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What are the 4 forces acting on a flying aircraft?

Drag, lift, push or pull, weight

4
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Lift is generated by _____ underneath a wing; this _____ lifts the wing

higher pressure, pressure

5
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Wake turbulence via wing-tip vortices is created as the air flows ____ from the _____

outward, body to the wingtip

6
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When air reaches the wingtip, the high pressure _____ towards low pressure, resulting in a twisting vortex of air that continues ______

rotates, in a downward spiral

7
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The strength of wing-tip vortices is governed by _____ and the _____ of an aircraft

shape of the wings, weight and speed

8
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Wing-tip vortices are most pronounced at _____

the wing-tips

9
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Wing-tip vortices show little dissipation within the first _____ of being produced. After ____, the dissipation rate will vary depending on factors.

2 minutes

10
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Wing-tip vortices on each side are ______ and ______ in shape.

counter-rotating, cylindrical

11
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Wing-tip vortices rotate _____ from the left-hand wing and _____ from the right-hand wing

clockwise, counter-clockwise

12
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Rotor-tip vortices are caused by the ______ of the blades and _______ to create intense, complex wake vortices

wing-like shape, rotation and forward motion

13
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Problems created by rotor-tip vortices are ______ than fixed-wing aircraft

generally greater

14
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The increased problems from rotor-tip vortices are because the helicopter’s lower operating speeds produce ________; the ______ has little bearing.

higher intensity wakes, size of the aircraft

15
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________ helicopters produce high-velocity vortices similar to wing-tip vortices

Departing or landing

16
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A jet engine thrust stream is the ______ created behind an aircraft’s jet stream

area of turbulence

17
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The wake turbulence from jet engine thrust stream is usually _____, but ______ and more dangerous the _____ you are to the aircraft.

extreme, relatively short, closer

18
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The jet wash/blast is greatest when power is increased to move the aircraft forward ______.

from a stopped position

19
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What is the jet blast intensity within 45 metres of the jet?

120 km/h

20
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Rotor downwash is the _____ created by helicopters ______.

downward turbulence, hovering or in forward flight

21
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The strength of rotor downwash depends on:

  • Helicopter weight

  • Air density

  • Forward speed

  • Rotor length

22
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Rotor downwash is greatest in ______ because _____.

hovering flight, airspeed is practically 0

23
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Once rotor downwash reaches the ground, it spreads out in all directions, causing _____.

severe buffetting

24
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Prop wash is turbulence created by _____

any propeller-driven aircraft

25
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Prop wash is based on the same principle as ______; but the effect is not as great

jet engine thrust stream

26
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Turbulence happens when the ____ under the wing meets the low pressure on top of the wing.

high pressure

27
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Aircraft flying directly into the core of a vortex will tend to _____ with the vortex. This is called _____.

roll, induced roll

28
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An aircraft’s capability to counteract an induced roll depends on its _____ and _____.

wingspan, responsiveness

29
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The smaller the aircraft that follows into the vortex in relation to the preceding aircraft that created it, the _______ and the _____ the following aircraft is to correct the uncommanded action.

more pronounced the effect, less likely

30
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When the ____ and ____ of a larger aircraft extend beyond the vortex, counter-roll control is usually effective and the effect of the induced roll can be minimized.

wingspan, ailerons

31
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Wing-tip vortices that are generated behind ______, or aircraft that descent to less than ______ above the runway, are subject to _____.

departing or arriving aircraft, 100 feet, ground effect

32
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In a no-wind situation, vortices that contact the ground tend to move ______, at a speed of about _____.

laterally outward, 5 knots

33
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A crosswind can move wing-tip vortices sideways with _____, which can increase or decrease respective vortices depending on their ____.

the direction of the wind, rotation

34
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A _____ or _____ can also change where the vortices begin or end in relation to the runway.

tailwind, headwind

35
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In calm or light wind conditions, wing-tip vortices can:

  • Remain in the touchdown area

  • Drift from aircraft operating on a nearby runway

  • Sink into take-off or landing paths from a crossing runway

  • Sink into the traffic pattern from other runway operations

  • Sink into the flight path of VFR flights at 500 feet AGL and below

36
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In calm and light wind conditions, wing-tip vortices can sink into the flight path of VFR flights at ______ and below.

500 feet AGL

37
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Which of these factors contributes to the strength of a wing-tip vortex?

All of these

38
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When is rotor downwash greatest?

When airspeed is low