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Full flight simulator study for evaluation of aircraft dynamics while encountering curved wake vortices

Vechtel, Dennis and Amelsberg, Swantje (2009) Full flight simulator study for evaluation of aircraft dynamics while encountering curved wake vortices. DLR-Interner Bericht. DLR-IB 111-2009/17, 46 S.

Full text not available from this repository.

Abstract

The CAE A330/A340 full flight simulator operated by the Zentrum für Flugsimulation Berlin (ZFB) is approved for training and research. While the certified JAA STD 1A (D-A-017) training software has its own dedicated host computer, research is activated by switching the host computer to an additional research computer.

Item URL in elib:https://elib.dlr.de/59639/
Document Type:Monograph (DLR-Interner Bericht)
Title:Full flight simulator study for evaluation of aircraft dynamics while encountering curved wake vortices
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vechtel, DennisUNSPECIFIEDUNSPECIFIED
Amelsberg, SwantjeUNSPECIFIEDUNSPECIFIED
Date:10 July 2009
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:46
Status:Published
Keywords:ZFB, Full flight simulator study, evaluation of aircraft dynamics, wake vortices
HGF - Research field:other
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By:INVALID USER
Deposited On:01 Oct 2009 13:31
Last Modified:08 Oct 2009 09:38

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