Zobrazeno 1 - 10
of 97
pro vyhledávání: '"Flugdynamik und Simulation"'
Autor:
Deiler, Christoph, Fezans, Nicolas
This paper presents the newest release (v0.52-beta) of the VIRTTAC-Castor flight dynamical simulation model. VIRTTAC-Castor is the first model of a larger family, VIRTTAC (Virtual Test Aircraft), developed at the DLR Institute of Flight Systems and f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::327b1a569316806a0b2ffa14a56ebbff
VIRTTAC-Castor is the first model of a larger family, VIRTTAC (Virtual Test Aircraft), developed at the DLR Institute of Flight Systems and freely available on GitHub. These models are black boxes in order to put the users in the situation of a fligh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f5b6ef48e92e52169b1e9967ae0872b3
Autor:
Diekmann, Jobst Henning
Publikováno v:
Journal of Aircraft. 56:1753-1764
This paper focuses on the flight mechanical characteristics of an active high-lift supported transport-type aircraft. The presented configuration combines a boundary-layer controlled flaps system with the benefits of propeller slipstream deflection.
Autor:
Fezans, Nicolas, Deiler, Christoph
Publikováno v:
SNE Simulation Notes Europe. 29:1-12
This paper presents the newly introduced Virtual Test Aircraft (VIRTTAC) model for use in benchmarks for aeronautics research. This model is shared in a black-box form and the core of an open-source benchmark suite. The model needs to remain undisclo
The Wake Vortex Prediction System WSVS (WirbelSchleppenVorhersageSystem) has been developed to tactically increase airport capacity by employing dynamically adjusted aircraft separations for approach and landing without compromising safety. For this
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7926126415ba0e63804da1ae40e1fb0f
https://elib.dlr.de/141251/
https://elib.dlr.de/141251/
Autor:
Ratzel, Michael
The Air Vehicle Simulator (AVES) is operated by the German Aerospace Center and provides a highly flexible platform with up to four different cockpit modules for research and development purposes. During the flight simulation, its visuals are created
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::8988090523f32c47e4266e9d624a7c2c
https://elib.dlr.de/140422/
https://elib.dlr.de/140422/
Autor:
Christoph Deiler
An evaluation of the effects of airframe icing on flight characteristics of fixed-wing aircraft is presented. The analysis is based on high-quality simulation models for different aircraft with distinct wing ice configurations (leading-edge and run-b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0d13e005b39101e0ca423852534958ba
https://elib.dlr.de/135051/
https://elib.dlr.de/135051/
Publikováno v:
CEAS Aeronautical Journal. 10:1033-1057
"This paper presents an overview of the DLR activities on active load alleviation in the CleanSky Smart Fixed Wing Aircraft project. The investigations followed two main research directions: the multi-objective, multi-model, structured controller des
Autor:
Christoph Deiler, Nicolas Fezans
A novel robust ice detection methodology for the early detection of icing-related flight performance degradation is presented. Based on data of 75,689 flights with modern commercial airliners, a maximum aircraft fleet's performance variation has been
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9a9a460b9f63b77e2a9fbc30536cfb9a
https://doi.org/10.2514/1.c034828
https://doi.org/10.2514/1.c034828
Autor:
Fezans, Nicolas, Vrancken, Patrick, Linsmayer, Philippe, Wallace, Christian, Deiler, Christoph
This paper gives an overview of the work performed by DLR on lidar-based gust load alleviation during the CleanSky and CleanSky 2 programmes. This work is put in relation with the work that was performed in the AWIATOR project, which is still the mos
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::59e9a96448cefbdbeaca2b9a70a06392
https://elib.dlr.de/134227/
https://elib.dlr.de/134227/