Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Marc Böswald"'
Publikováno v:
Materials & Design, Vol 207, Iss , Pp 109885- (2021)
Constrained layer damping treatments have been commonly used for vibration damping. The included viscoelastic material exhibits high damping potential that is retrieved under shear deformation. However, the impact of temperature on the viscoelastic p
Externí odkaz:
https://doaj.org/article/543dc16eb5d041f5b5f0686bad5ffc93
Publikováno v:
INTER-NOISE and NOISE-CON Congress and Conference Proceedings. 265:2288-2297
The wings of passenger aircrafts are constantly vibrating due to various loads. There are transient low-frequency vibrations caused by gust loads. But there are also higher-frequency vibrations caused by the vibration load of the jet engines. The hig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9cbcb137aeccf25c3a75d7945b86aeca
https://doi.org/10.3397/in_2022_0327
https://doi.org/10.3397/in_2022_0327
Autor:
Keith Soal, Robin Volkmar, Carsten Thiem, Julian Sinske, Yasser M. Meddaikar, Yves Govers, Marc Böswald, Daniel Teubl, Julius Bartasevicius, Mihaly Nagy, Balint Vanek
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5e556c9ca50d49b5533962fa1d8c487
https://doi.org/10.2514/6.2023-0373
https://doi.org/10.2514/6.2023-0373
Publikováno v:
INTER-NOISE and NOISE-CON Congress and Conference Proceedings. 263:1712-1722
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts are a necessity for long term sustainable air travel. These concepts pose new challenges for the vibro-acoustic assessment of cabin structures and the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::240b6a7c6166f5c4f7313b06a2345177
https://doi.org/10.3397/in-2021-1906
https://doi.org/10.3397/in-2021-1906
Publikováno v:
CEAS Aeronautical Journal. 12:413-426
In this paper, the effect of nonlinear actuator dynamics on the performance of an active load alleviation system for an experimental flexible wing is studied. Common nonlinearities such as backlash or rate limits are considered for the control surfac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b619a5ee3a3c187fc1feaa9f71f71a4
https://doi.org/10.1007/s13272-021-00504-y
https://doi.org/10.1007/s13272-021-00504-y
Publikováno v:
Jelicic, G, Böswald, M & Brandt, A 2021, ' Improved computation in terms of accuracy and speed of LTI system response with arbitrary input ', Mechanical Systems and Signal Processing, vol. 150, 107252 . https://doi.org/10.1016/j.ymssp.2020.107252
Spectral analysis and system identification techniques require suitably long data sets. Linear time-invariant (LTI) systems under random input can be demanding in terms of accurate simulation of all dynamics because of calculation time. This paper de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::924c5c8598a1c709fafbf3ea8d59c160
https://elib.dlr.de/139811/
https://elib.dlr.de/139811/
Publikováno v:
Marine Structures. 79:103043
Accurate dynamic models of flexible ship structures are required to predict structural vibration caused by environmental loads. Knowledge of dynamic or modal properties are important, for example, to study fatigue damage. In this paper, operational m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cdb5aaa16c6c3c713bfe2a873d9a9d3c
https://doi.org/10.1016/j.marstruc.2021.103043
https://doi.org/10.1016/j.marstruc.2021.103043
Publikováno v:
Journal of Sound and Vibration. 400:457-480
Aircraft structures are characterized by their lightweight design. As such, they are prone to vibrations. Numerical models based on the Finite Element Method often show significant deviations when the mid-frequency range is considered, where strong i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::31149ad83766df3987bc805d98aed0d4
https://doi.org/10.1016/j.jsv.2017.04.024
https://doi.org/10.1016/j.jsv.2017.04.024
Autor:
Julian Springer, Jan Schwochow, Marc Böswald, Julian Sinske, G. Jelicic, Ralf Buchbach, Yves Govers
Publikováno v:
Scopus-Elsevier
University of Southern Denmark
University of Southern Denmark
The work presented in this paper shows a simple way how to obtain eigenfrequencies, damping ratios and mode shapes of an aircraft prototype. The only prerequisite is flight test instrumentation (FTI) including a set of acceleration sensors with suffi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::763434993003304052f9ad028ec3afa4
https://elib.dlr.de/115585/
https://elib.dlr.de/115585/