Zobrazeno 1 - 10
of 151
pro vyhledávání: '"M, Liersch"'
Publikováno v:
CEAS Aeronautical Journal. 11:781-802
This article belongs to a series of publications on the design and assessment of the MULDICON UCAV configuration. MULDICON is a 53° swept flying wing combat aircraft concept, investigated in a common effort between the DLR research project Mephisto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cac508feb61587f7b44cfa27d00dc068
https://doi.org/10.1007/s13272-020-00453-y
https://doi.org/10.1007/s13272-020-00453-y
Publikováno v:
Journal of Aircraft. 55:454-474
The ability to accurately predict both static and dynamic stability characteristics of air vehicles using computational fluid dynamics methods could revolutionize the air vehicle design process, especially for military air vehicles. A validated compu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::571645f7a7ab108bc58a7073b53677f7
https://doi.org/10.2514/1.c033808
https://doi.org/10.2514/1.c033808
Autor:
Kathrin Schaffert, Pier Davide Ciampa, Robert Mischke, Stefan Goertz, Erwin Moerland, Alexander Weinert, Brigitte Boden, Jan Flink, Annika Wohlan, Caslav Ilic, Carsten M. Liersch, Tobias Wunderlich
Publikováno v:
AIAA Aviation 2019 Forum.
DLR's Remote Component Environment (RCE) is an open-source software environment for defining and executing workflows containing distributed simulation tools by integrating them into a peer-to-peer network. It is being developed primarily by DLR and h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::eeced5d13a27b67fd00f65b999f48d4e
https://doi.org/10.2514/6.2019-2989
https://doi.org/10.2514/6.2019-2989
Publikováno v:
Aerospace Science and Technology. 107:106232
The extensive amount of aerodynamic data needed for the creation of a Stability & Control data set requires efficient and reliable tools. For this reason, the task of producing a large and dense data set in general relies on ground-facility testing a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d333852adb4c12bdd357a97d943b3db
https://doi.org/10.1016/j.ast.2020.106232
https://doi.org/10.1016/j.ast.2020.106232
Autor:
Russell M. Cummings, Carsten M. Liersch, Ryan G. Maye, Jan Vormweg, T.L. Jeans, Andreas Schütte
Publikováno v:
Aerospace Science and Technology. 99:105764
This article belongs to a series of publications about the activities performed within the NATO STO Research Task Group AVT-251 on “Multi-Disciplinary design and performance assessment of effective, agile NATO Air Vehicles”. The article concentra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f20442345ce7580f975d6086917e3e14
https://doi.org/10.1016/j.ast.2020.105764
https://doi.org/10.1016/j.ast.2020.105764
Autor:
Carsten M. Liersch, Gertjan Looye, Yasim Julian Hasan, Thomas Klimmek, Jan Flink, Sebastian Freund, Erwin Moerland, Till Pfeiffer, Richard Kuchar, Mario Schrader, Sebastian Zenkner
This paper provides an overview of current activities of DLR (German Aerospace Center) with respect to stability and control investigations in the context of early stages of aircraft design. For this purpose, DLR follows an interdisciplinary and mult
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1062a872ee9cfec949f10d40080f38f5
https://elib.dlr.de/120770/
https://elib.dlr.de/120770/
Publikováno v:
2018 Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1165239385fb80e3fbb09ff5b675dcb3
https://doi.org/10.2514/6.2018-3329
https://doi.org/10.2514/6.2018-3329
Autor:
Carsten M. Liersch, Julian Scherer, Carsten Klein, Daniel Böhnke, Jan Flink, Yasim Julian Hasan, Sebastian Freund, Erwin Moerland, Jonas Jepsen, Till Pfeiffer, Gabriel Pinho Chiozzotto
Publikováno v:
17th AIAA Aviation Technology, Integration, and Operations Conference.
Due to its drag saving potential through application of high aspect ratio wings, the strut-braced wing configuration is considered a promising candidate as a next generation single-aisle aircraft. This potential is reflected in the results of the ren
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb11488945985f7319dd467a10c5825e
https://doi.org/10.2514/6.2017-4397
https://doi.org/10.2514/6.2017-4397