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Mitigating Aircraft Wake Vortex Risks During Final Approach via Plate Lines

Holzäpfel, Frank (2021) Mitigating Aircraft Wake Vortex Risks During Final Approach via Plate Lines. 9th International Conference on Vortex Flow Mechanics, 2021-10-11 - 2021-10-13, Virtuelle Konferenz.

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As an unavoidable consequence of lift, every flying vehicle generates counter-rotating regions of turbulence known as wake vortices. These long-lived trailing vortices constitute a potential threat to following air traffic. Aircraft must therefore keep to a predetermined minimum separation distance. These aircraft separations limit the capacity of congested airports in a basically rapidly growing aeronautical environment. Decades of research on effective aircraft modifications aiming at the alleviation of the wake vortex hazard did not lead to operational use until today. The highest risk to encounter wake vortices prevails in ground proximity, where the vortices cannot descend below the glide path but tend to rebound due to the interaction with the ground surface. Weak crosswinds may compensate the self-induced lateral propagation of the upwind vortex, such that it may hover over the runway directly in the flight path of the following aircraft. That’s why aircraft experience wake vortex encounters time after time, even under adherence to separation standards. So-called plate lines mitigate the risk of wake vortex encounters during final approach and may help to enhance runway capacity. One plate line consists of several upright plates that are installed underneath the approach glide path at the ends of runways. Plate lines are passive, cost-effective, robust and safe. Since the first idea developed in the year 2008, the functionality of the patented plate lines was first demonstrated in towing tank experiments. Next, using high-performance numerical simulations, the underlying physical mechanism was analyzed in detail, the size of the plate lines was optimized, and the influence of wind was investigated. Flight tests with the DLR research aircraft HALO (Gulfstream G550) at the special airport Oberpfaffenhofen showed that the lifetime of the longest-lived vortices can be reduced by about 30%. When a vortex gets close to the plates, strong omega-shaped secondary vortices are induced at the plate’s surface that actively approach the wake vortices by self-induced motion. Then the secondary vortices are wrapped around the wake vortices by the primary wake vortex flow. Finally, the secondary vortices propagate along either side of the wake vortices again driven by self-induced motion and accelerate their decay. In the year 2019, the effectivity of the plate lines was demonstrated in a large-scale measurement campaign at Vienna International Airport. Two temporary plate lines were installed underneath the glide path to runway 16. During a six-month period, wake vortex decay was measured for 9473 landings using lidar. It was found that plate lines reduce the lifetime of the most safety-relevant wake vortices by 22% for Medium category aircraft and by up to 37% for Heavy category aircraft. Depending on the aircraft pairing, plate lines allow for a potential separation reduction of 12% to 20% compared to the RECAT-EU separation scheme.

Item URL in elib:https://elib.dlr.de/146281/
Document Type:Conference or Workshop Item (Speech)
Title:Mitigating Aircraft Wake Vortex Risks During Final Approach via Plate Lines
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Holzäpfel, FrankDLR, IPAhttps://orcid.org/0000-0003-3182-1832UNSPECIFIED
Date:13 October 2021
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:wake vortex, vortex mitigation, approach and landing, plate lines
Event Title:9th International Conference on Vortex Flow Mechanics
Event Location:Virtuelle Konferenz
Event Type:international Conference
Event Start Date:11 October 2021
Event End Date:13 October 2021
Organizer:University of Patras, Greece
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Air Transportation and Impact
DLR - Research area:Aeronautics
DLR - Program:L AI - Air Transportation and Impact
DLR - Research theme (Project):L - Climate, Weather and Environment
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Atmospheric Physics > Transport Meteorology
Deposited By: Holzäpfel, Dr. habil. Frank
Deposited On:26 Nov 2021 13:03
Last Modified:24 Apr 2024 20:45

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