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Aircraft Wake Vortex State-of-the-Art & Research Needs, Kapitel 5.5 Encounter Mechanisms and Simulation

Luckner, Robert and Bieniek, David and Bauer, Tobias and Fischenberg, Dietrich and Schwarz, Carsten and Vechtel, Dennis (2015) Aircraft Wake Vortex State-of-the-Art & Research Needs, Kapitel 5.5 Encounter Mechanisms and Simulation. Project Report.

Full text not available from this repository.

Official URL: http://wakenet.eu/index.php?id=191

Abstract

The complex physical process of the wake vortex encounter (WVE) mechanism - from vortex generation to encounter hazard - is modelled by linking several sub-models. The overall process model is suited to determine the conditions for which modified separation minima are safe and can be applied to risk assessments that are needed to revise wake turbulence separation standards as well as for evaluation of new operational ATC concepts. Parts of this overall model can be used for other applications, such as real-time flight simulations to investigate WVE physics or for the development of vortex detection, warning and avoidance (DWA) systems for onboard and on-ground applications.

Item URL in elib:https://elib.dlr.de/100595/
Document Type:Monograph (Project Report)
Title:Aircraft Wake Vortex State-of-the-Art & Research Needs, Kapitel 5.5 Encounter Mechanisms and Simulation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Luckner, RobertTU BerlinUNSPECIFIED
Bieniek, DavidTU BerlinUNSPECIFIED
Bauer, TobiasFT-FDSUNSPECIFIED
Fischenberg, DietrichFT-FDSUNSPECIFIED
Schwarz, CarstenFT-FDSUNSPECIFIED
Vechtel, DennisFT-FDSUNSPECIFIED
Date:10 November 2015
Journal or Publication Title:Aircraft Wake Vortex State-of-the-Art & Research Needs
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.17874/BFAEB7154B0
Number of Pages:19
Editors:
EditorsEmail
Holzäpfel, FrankDLR-PA
Reinke, Andreasandreas.a.reinke@airbus.com
Schwarz, CarstenDLR-FT-FDS
Status:Published
Keywords:wake vortex encounter, flight simulation, encounter modelling, aircraft reaction, aerodynamic interaction models, pilot behaviour models, severity assessment
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Bauer, Tobias
Deposited On:02 Feb 2016 14:59
Last Modified:10 May 2016 23:37

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