TY - CHAP A1 - Michel, P. A1 - Zilligen, H. A1 - Rosin, J. A1 - Butenweg, Christoph T1 - Seismisches Verhalten pfahlgegründeter Tankbauwerke T2 - Erdbeben und bestehende Bauten : 14. D-A-C-H Tagung 20.08. - 21.08.2015, ETH Zürich. (Dokumentation / SIA ; D 0255) Y1 - 2015 SN - 978-3-03732-060-0 SP - 181 EP - 188 PB - SGEB CY - Zürich ER - TY - JOUR A1 - Taddei, Francesca A1 - Butenweg, Christoph A1 - Klinkel, S. T1 - Parametric investigation of the soil-structure interaction effects on the dynamic behaviour of a shallow foundation supported wind turbine considering a layered soil JF - Wind energy : an international journal for progress and applications in wind power conversion technology Y1 - 2015 U6 - https://doi.org/10.1002/we.1703 SN - 1099-1824 (E-Journal); 1095-4244 (Print) VL - Volume 18 IS - Issue 3 SP - 399 EP - 417 PB - Wiley CY - Weinheim ER - TY - JOUR A1 - Kubalski, Thomas A1 - Butenweg, Christoph T1 - Modelling strategies for horizontally loaded infill masonry T1 - Modellierungsansätze für horizontal beanspruchtes Ausfachungsmauerwerk JF - Mauerwerk : European journal of masonry Y1 - 2015 U6 - https://doi.org/10.1002/dama.201500675 VL - Volume 19 IS - Issue 5 SP - 363 EP - 369 PB - Wiley CY - Weinheim ER - TY - CHAP A1 - Peloni, Alessandro A1 - Ceriotti, Matteo A1 - Dachwald, Bernd T1 - Solar-Sailing Trajectory Design for Close-up NEA Observations Mission T2 - 4th IAA Planetary Defense Conference - PDC 2015, 13-17 April 2015, Frascati, Roma, Italy Y1 - 2015 N1 - IAA-PDC-15-P-19 ER - TY - CHAP A1 - Peloni, A. A1 - Ceriotti, M. A1 - Dachwald, Bernd T1 - Preliminary trajectory design of a multiple NEO rendezvous mission through solar sailing T2 - Proceedings of the International Astronautical Congress, IAC, Vol. 8, 2014 Y1 - 2015 SN - 978-1-63439-986-9 SP - 5352 EP - 5366 PB - Curran CY - Red Hook, NY ER - TY - CHAP A1 - Digel, Ilya A1 - Sadykov, R. A1 - Temiz Artmann, Aysegül A1 - Artmann, Gerhard T1 - Changes in intestinal microflora in rats induced by oral exposure to low lead (II) concentrations T2 - Lead Exposure and Poisoning: Clinical Symptoms, Medical Management and Preventive Strategies Y1 - 2015 SN - 9781634826990 SP - 75 EP - 99 PB - Nova Science Publ. ER - TY - JOUR A1 - Akimbekov, Nuraly S. A1 - Digel, Ilya A1 - O’Heras, C. A1 - Tastambek, K.T. A1 - Savitskaya, I.S. A1 - Ualyeva, P.S. A1 - Mansurov, Z.A. A1 - Zhubanova, A.A. T1 - Adsorption of bacterial lipopol ysaccharides on carbonized ri ce husks obtained in the batch experiments JF - KazNU Bulletin. Biology series Y1 - 2015 SN - 1563-0218 VL - 60 IS - No 1/2 SP - 144 EP - 148 ER - TY - CHAP A1 - Grundmann, Jan Thimo A1 - Bauer, Waldemar A1 - Biele, Jens A1 - Cordero, Frederico A1 - Dachwald, Bernd A1 - Koncz, Alexander A1 - Krause, Christian A1 - Mikschl, Tobias A1 - Montenegro, Sergio A1 - Quantius, Dominik A1 - Ruffer, Michael A1 - Sasaki, Kaname A1 - Schmitz, Nicole A1 - Seefeldt, Patric A1 - Tóth, Norbert A1 - Wejmo, Elisabet T1 - From Sail to Soil – Getting Sailcraft Out of the Harbour on a Visit to One of Earth’s Nearest Neighbours T2 - 4th IAA Planetary Denfense Conference - PDC 2015, 13-17 April 2015, Frascati, Roma, Italy Y1 - 2015 ER - TY - RPRT A1 - Damm, Marc André A1 - Anthrakidis, Anette A1 - Fend, Thomas T1 - Partikelminderungssystem mit einstellbarem Partikelrückhaltegrad : Varytrap : Schlussbericht : Laufzeit: 01.07.2010-28.02.2014 Y1 - 2015 U6 - https://doi.org/10.2314/GBV:848651863 N1 - Report-Nr: 17012X10 CY - Jülich ER - TY - CHAP A1 - Pirovano, Laura A1 - Seefeldt, Patric A1 - Dachwald, Bernd A1 - Noomen, Ron T1 - Attitude and orbital modeling of an uncontrolled solar-sail experiment in low-Earth orbit T2 - 25th International Symposium on Space Flight Dynamics ISSFD N2 - Gossamer-1 is the first project of the three-step Gossamer roadmap, the purpose of which is to develop, prove and demonstrate that solar-sail technology is a safe and reliable propulsion technique for long-lasting and high-energy missions. This paper firstly presents the structural analysis performed on the sail to understand its elastic behavior. The results are then used in attitude and orbital simulations. The model considers the main forces and torques that a satellite experiences in low-Earth orbit coupled with the sail deformation. Doing the simulations for varying initial conditions in attitude and rotation rate, the results show initial states to avoid and maximum rotation rates reached for correct and faulty deployment of the sail. Lastly comparisons with the classic flat sail model are carried out to test the hypothesis that the elastic behavior does play a role in the attitude and orbital behavior of the sail KW - Solar sail KW - Gossamer structures KW - Attitude dynamics KW - Orbital dynamics Y1 - 2015 N1 - 25th International Symposium on Space Flight Dynamics ISSFD October 19 – 23, 2015, Munich, Germany https://issfd.org/2015/ SP - 1 EP - 15 ER -