Turbulence that follows behind aircraft traveling through air
Wake turbulence is a disturbance in the
atmosphere that forms behind an
aircraft as it passes through the air. It includes several components, the most significant of which are
wingtip vortices and jet-wash, the rapidly moving gases expelled from a jet engine.
Wake turbulence is especially hazardous in the region behind an aircraft in the
takeoff or
landing phases of flight. During take-off and landing, an aircraft operates at a high
angle of attack. This
flight attitude maximizes the formation of strong vortices. In the vicinity of an airport, there can be multiple aircraft, all operating at low speed and low altitude; this provides an extra risk of wake turbulence with a reduced height from which to recover from any upset.[1]
Definition
Wake turbulence is a type of
clear-air turbulence. In the case of wake turbulence created by the wings of a heavy aircraft, the rotating vortex-pair lingers for a significant amount of time after the passage of the aircraft, sometimes more than a minute. One of these rotating vortices can seriously upset or even invert a smaller aircraft that encounters it, either in the air or on the ground.[citation needed]
In fixed-wing level flight
The vortex circulation is outward, upward, and around the wingtips when viewed from either ahead or behind the aircraft. Tests with large aircraft have shown that vortices remain spaced less than a wingspan apart, drifting with the wind, at altitudes greater than a wingspan from the ground. Tests have also shown that the vortices sink at a rate of several hundred feet per minute, slowing their descent and diminishing in strength with time and distance behind the generating aircraft.[2]
At altitude, vortices sink at a rate of 90–150 m (300–490 ft) per minute and stabilize about 150–270 m (490–890 ft) below the
flight level of the generating aircraft. Therefore, aircraft operating at altitudes greater than 600 m (2,000 ft) are considered to be at less risk.[3]
When the vortices of larger aircraft sink close to the ground — within 100–200 ft (30–61 m) — they tend to move laterally over the ground at a speed of 2–3 kn (3.7–5.6 km/h; 2.3–3.5 mph). A crosswind decreases the lateral movement of the upwind vortex and increases the movement of the downwind vortex.[4]
Helicopters
Helicopters also produce wake turbulence. Helicopter wakes may be significantly stronger than those of a fixed-wing aircraft of the same weight. The strongest wake will occur when the helicopter is operating at slower speeds (20 to 50
knots). Light helicopters with two-blade rotor systems produce a wake as strong as heavier helicopters with more than two blades. The strong rotor wake of the
Bell Boeing V-22 Ospreytiltrotor can extend further and has
contributed to a crash.[5]
Hazard avoidance
Wingtip devices may slightly lessen the power of
wingtip vortices. However, such changes are not significant enough to change the distances or times at which it is safe to follow other aircraft.[6]
ICAO mandates wake turbulence categories based upon the
maximum takeoff weight (MTOW) of the aircraft. These are used for separation of aircraft during take-off and landing.
There are a number of separation criteria for take-off, landing, and en-route phases of flight based upon wake turbulence categories.
Air Traffic Controllers will sequence aircraft making
instrument approaches with regard to these criteria. The aircraft making a visual approach is advised of the relevant recommended spacing and are expected to maintain their separation.[7]: 9
Parallel or crossing runways
During takeoff and landing, an aircraft's wake sinks toward the ground and moves laterally away from the runway when the wind is calm. A three-to-five-knot (3–6 mph; 6–9 km/h) crosswind will tend to keep the upwind side of the wake in the runway area and may cause the downwind side to drift toward another
runway. Since the wingtip vortices exist at the outer edge of an airplane's wake, this can be dangerous. [7]: 10
Uncommanded aircraft movements (such as wing rocking) may be caused by wake. This is why maintaining situational awareness is critical. Ordinary turbulence is not unusual, particularly in the approach phase. A pilot who suspects wake turbulence is affecting his or her aircraft should get away from the wake, execute a
missed approach or
go-around and be prepared for a stronger wake encounter. The onset of wake can be subtle and even surprisingly gentle. There have been serious accidents (see the next section) where pilots have attempted to salvage a landing after encountering moderate wake only to encounter severe wake turbulence that they were unable to overcome. Pilots should not depend on any aerodynamic warning, but if the onset of wake is occurring, immediate evasive action is vital.
Plate lines
In 2020, researchers looked into installing "plate lines" near the runway threshold to induce secondary vortices and shorten the vortex duration. In the trial installation at
Vienna International Airport, they reported a 22%-37% vortex reduction.[9][10]
8 June 1966 – an
XB-70 collided with an
F-104. Though the true cause of the collision is unknown, it is believed that due to the
XB-70 being designed to have enhanced wake turbulence to increase lift, the F-104 moved too close, therefore getting caught in the vortex and colliding with the wing (see
main article).
A DC-9 crashed at the
Greater Southwest International Airport while performing "touch and go" landings behind a
DC-10. This crash prompted the FAA to create new rules for minimum following separation from "heavy" aircraft.[11]
16 Jan 1987 – A
Yakovlev Yak-40 crashed just after
take-off in Tashkent. The flight took off just one minute fifteen seconds after an
Ilyushin Il-76, thus encountering its
wake vortex. The Yakovlev Yak-40 then banked sharply to the right, struck the ground, and caught fire. All nine people on board
Aeroflot Flight 505 died.[12]
15 December 1993 – A chartered aircraft with five people on board, including
In-N-Out Burger president Rich Snyder, crashed several miles before
John Wayne Airport in Orange County, California. The aircraft was following a
Boeing 757 for landing when it became caught in its wake turbulence, rolled into a deep descent, and crashed. As a result of this and other incidents involving aircraft following behind a Boeing 757, the FAA now employs the separation rules of heavy aircraft for the Boeing 757.
8 September 1994 –
USAir Flight 427 crashed near
Pittsburgh, Pennsylvania. This accident was believed to involve wake turbulence, though the primary cause was a defective rudder control component which caused the aircraft to react abnormally to the pilots' control inputs prompted by the wake encounter.
20 September 1999 – A
JAS 39A Gripen from Airwing F 7 Såtenäs crashed into
Lake Vänern in Sweden during an air combat maneuvering exercise. After passing through the wake vortex of the other aircraft, the Gripen abruptly changed course. Before the Gripen impacted the ground, the pilot ejected from the aircraft and landed safely by parachute in the lake.
8 July 2008 – A
United States Air ForcePC-12 trainer crashed at
Hurlburt Field, Fla., when the pilot tried to land too closely behind a larger AC-130U Spooky gunship and was caught in the gunship's wake turbulence. Air Force rules require at least a two-minute separation between slow-moving heavy planes like the AC-130U and small, light planes, but the PC-12 trailed the gunship by only about 40 seconds. As the PC-12 hit the wake turbulence, it suddenly rolled to the left and began to turn upside down. The instructor pilot stopped the roll, but before he could get the plane upright, the left wing struck the ground, sending the plane skidding 669 ft (204 m) across a field before stopping on a paved overrun.[14]
3 November 2008 – The wake turbulence of an
Airbus A380-800 caused temporary loss of control to a
Saab 340 on approach to a parallel runway during high crosswind conditions.[15]
4 November 2008 – In the
2008 Mexico City plane crash, a
Learjet 45 carrying Mexican Interior Secretary
Juan Camilo Mouriño crashed near
Paseo de la Reforma Avenue when turning for final approach to runway 05R at
Mexico City International Airport. The airplane was flying behind a 767-300 and above a heavy helicopter. According to the Mexican government, the pilots were not told about the type of plane that was approaching before them, nor did they reduce to minimum approach speed.[citation needed]
9 September 2012 – A
Robin DR 400 crashed after rolling 90 degrees in wake turbulence induced by the preceding
Antonov An-2. Three were killed and one was severely injured.[16][17]
28 March 2014 – An
Indian Air ForceC-130J-30 KC-3803 crashed near
Gwalior, India, killing all five personnel aboard.[18][19][20] The aircraft was conducting low level penetration training by flying at around 300 ft (90 m) when it ran into wake turbulence from another C-130J aircraft that was leading the formation, causing it to crash.[21][22]
7 January 2017 – A private
Bombardier Challenger 604 rolled three times in midair and dropped 10,000 ft (3,000 m) after encountering wake turbulence when it passed 1,000 ft (300 m) under an
Airbus A380 over the Arabian Sea. Several passengers were injured, one seriously. Due to the G-forces experienced, the plane was damaged beyond repair and was consequently written off.[23]
14 June 2018 – At 11:29 pm,
Qantas passenger flight QF94, en route from Los Angeles to Melbourne, suffered a sudden freefall over the ocean after lift-off as a result of an intense wake vortex. The event lasted for about ten seconds, according to the passengers. The turbulence was caused by the wake of the previous Qantas flight QF12, which had departed only two minutes before flight QF94.[24]
Measurement
Wake turbulence can be measured using several techniques. Currently, ICAO recognizes two methods of measurement, sound tomography, and a high-resolution technique, the
Dopplerlidar, a solution now commercially available. Techniques using
optics can use the effect of turbulence on
refractive index (
optical turbulence) to measure the distortion of light that passes through the turbulent area and indicate the strength of that turbulence.
Wake turbulence can occasionally, under the right conditions, be heard by ground observers.[25] On a still day, the wake turbulence from heavy jets on landing approach can be heard as a dull roar or whistle. This is the strong core of the vortex. If the aircraft produces a weaker vortex, the breakup will sound like tearing a piece of paper. Often, it is first noticed some seconds after the direct noise of the passing aircraft has diminished. The sound then gets louder. Nevertheless, being highly directional, wake turbulence sound is easily perceived as originating a considerable distance behind the aircraft, its apparent source moving across the sky just as the aircraft did. It can persist for 30 seconds or more, continually changing timbre, sometimes with swishing and cracking notes, until it finally dies away.
In the 1986 film Top Gun, Lieutenant Pete "Maverick" Mitchell, played by
Tom Cruise, suffers two
flameouts caused by passing through the jetwash of another aircraft, piloted by fellow aviator Tom "Ice Man" Kazansky (played by
Val Kilmer). As a result, he is put into an unrecoverable spin and is forced to eject, killing his RIO Nick "Goose" Bradshaw.[26] In a subsequent incident, he is caught in an enemy fighter's jetwash, but manages to recover safely.
In the movie Pushing Tin, air traffic controllers stand just off the threshold of a runway while an aircraft lands in order to experience wake turbulence firsthand. However, the film dramatically exaggerates the effect of turbulence on persons standing on the ground, showing the protagonists being blown about by the passing aircraft. In reality, the turbulence behind and below a landing aircraft is too gentle to knock over a person standing on the ground. (In contrast,
jet blast from an aircraft taking off can be extremely dangerous to people standing behind the aircraft.)
^"Aircraft Wake Turbulence". U.S. Department of Transportation Federal Aviation Administration. AC No: 90-23G. February 10, 2014. p. 24. Retrieved 2023-03-05.