TY - CHAP A1 - Usai, Pierpaolo A1 - Corucci, Alessandro A1 - Gligorevic, Snjezana A1 - Monorchio, Agostino T1 - Estimation of airport surface propagation channel: ray tracing model and measurements T2 - Proceedings of the 5th European Conference on Antennas and Propagation (EUCAP) : 11 - 15 April 2011, Rome, Italy Y1 - 2011 SN - 978-1-4577-0250-1 SP - 1634 EP - 1638 ER - TY - CHAP A1 - Tran, Thanh Ngoc A1 - Novacek, V. A1 - Tolba, R. A1 - Klinge, U. A1 - Turquier, F. A1 - Staat, Manfred T1 - Experimental and Computational approach to study colorectal anastomosis. ISB2011, Proceedings of the XXIII Congress of the International Society of Biomechanics, Brussels, Belgium, July 3-7, 2011 N2 - Summary: This paper presents a methodology to study and understand the mechanics of stapled anastomotic behaviors by combining empirical experimentation and finite element analysis. Performance of stapled anastomosis is studied in terms of leakage and numerical results which are compared to in vitro experiments performed on fresh porcine tissue. Results suggest that leaks occur between the tissue and staple legs penetrating through the tissue. KW - Anastomose KW - Finite-Elemente-Methode KW - Biomechanik KW - Anastomosis KW - Finite element method KW - Biomechanics Y1 - 2011 ER - TY - CHAP A1 - Thenent, N. E. A1 - Dahmann, Peter T1 - Increasing aircraft design flexibility ‐ The development of a hydrostatic transmission for gliders with self‐launching capability T2 - Deutscher Luft- und Raumfahrtkongress 2011 : Bremen, 27. bis 29. September 2011 ; Tagungsband Y1 - 2011 SN - 978-3-9321-8274-7 SP - 865 EP - 883 PB - Dt. Gesellschaft für Luft- und Raumfahrt CY - Bonn ER - TY - CHAP A1 - Thenent, N. E. A1 - Dahmann, Peter T1 - Hydrostatic propeller drive T2 - Proceedings of the conference : 18 - 20 May, 2011 Tampere, Finland / the Twelth Scandinavian International Conference on Fluid Power, SICFP'11. Ed.: Harri Sairiala ... Vol. 1 Y1 - 2011 SN - 978-952-15-2517-9 SP - 217 EP - 227 CY - Tampere ER - TY - CHAP A1 - Teixeira Boura, Cristiano José A1 - Eckstein, J. A1 - Felinks, J. A1 - Göttsche, Joachim A1 - Hoffschmidt, Bernhard A1 - Schmitz, S. T1 - 3-D CFD simulation of an air-sand heat exchanger T2 - SolarPACES 2011 : concentrating solar power and chemical energy systems : 20 - 23 September, 2011, Granada, Spain Y1 - 2011 CY - Granada ER - TY - CHAP A1 - Taddei, Francesca A1 - Reindl, Lukas A1 - Park, Jin A1 - Butenweg, Christoph A1 - Karadogan, Faruk T1 - Numerical investigation of AAC wall panels based on the damage plasticity constitutive law T2 - Cement, Wapno, Beton ; 2011, 7, Special issue: 5th International Conference on Autoclaved Aerated Concrete 'Securing a sustainable future' to be held at Bydgoszcz to celebrate 60 years of AAC experience in Poland, Bydgoszcz, September 14-17, 2011 Y1 - 2011 SN - 1425-8129 SP - 86 EP - 91 PB - Stowarzyszenie Producentów Cementu i Wapna CY - Krakow ER - TY - CHAP A1 - Stieglitz, Kristian A1 - Wollert, Jörg T1 - Approach of using ultra-wideband-radio in industrial real-time ethernet networks T2 - The 4th International Multi-Conference on Engineering and Technological Innovation : IMETI : July 19th - July 22nd, 2011, Orlando, Florida, USA Y1 - 2011 SP - 1 EP - 6 ER - TY - CHAP A1 - Siekmann, Thomas A1 - Müller, Karsten T1 - Adaptive potential of the stormwater management in urban areas faced by the climate change T2 - 12th International Conference on Urban Drainage, Porto Alegre/Brazil, 11-16 September 2011 Y1 - 2011 ER - TY - CHAP A1 - Schneckenburger, N. A1 - Franzen, N. A1 - Gligorevic, Snjezana A1 - Schnell, M. T1 - L-band compatibility of LDACS1 T2 - IEEE/AIAA 30th Digital Avionics Systems Conference (DASC) : 16 - 20 Oct. 2011, Seattle, Wash. Y1 - 2011 SN - 978-1-61284-797-9 SN - 2155-7195 SP - 4C3-1 EP - 4C3-11 ER - TY - CHAP A1 - Schiffer, Stefan A1 - Ferrein, Alexander A1 - Lakemeyer, Gerhard T1 - Fuzzy representations and control for domestic service robots in Golog T2 - Intelligent robotics and applications : 4th International conference, ICIRA 2011, Aachen, Germany, December 6-8, 2011, proceedings, part I. (Lecture notes in computer science ; 7102) Y1 - 2011 SN - 978-3-642-25486-4 SP - 241 EP - 250 ER - TY - CHAP A1 - Sauerborn, Markus T1 - Investigations to the influence of clouds and aerosols to the haze of the sunshape T2 - SolarPACES 2011 : concentrating solar power and chemical energy systems : 20 - 23 September, 2011, Granada, Spain Y1 - 2011 CY - Granada ER - TY - CHAP A1 - Reisgen, Uwe A1 - Schleser, Markus A1 - Scheik, Sven A1 - Michaeli, Walter A1 - Grönlund, Oliver A1 - Neuß, Andreas A1 - Wunderle, Johannes A1 - Poprawe, Reinhart A1 - Rösner, A. A1 - Bobzin, Kirsten A1 - Schläfer, Thomas A1 - Theiß, Sebastian A1 - Kutschmann, Pia A1 - Haberstroh, Edmund A1 - Flock, Dustin A1 - Bührig-Polaczek, Andreas A1 - Jakob, M. ED - Thoben, Klaus-Dieter T1 - Novel process chains for the production of plastics/metal-hybrids T2 - 17th International Conference on Concurrent Enterprising (ICE 2011) : Aachen, Germany, 20 - 22 June 2011 Y1 - 2011 SN - 978-1-457-70772-8 ; 978-3-943024-05-0 SP - 596 EP - 604 PB - IEEE CY - Piscataway, NJ ER - TY - CHAP A1 - Reisgen, Uwe A1 - Schleser, Markus A1 - Abdurakhmanov, Aydemir A1 - Turichin, Gleb A1 - Valdaitseva, Elena A1 - Bach, Friedrich-Wilhelm A1 - Hassel, Thomas A1 - Beniyashi, Alexander T1 - Investigation of factors for defect-free weld formation by non-vacuum electron beam welding T2 - Laser technologies in welding and materials processing : proceedings of the fifth international conference, 24 - 27 May 2011, Katsiveli, Crimea, Ukraine Y1 - 2011 SP - 104 EP - 109 PB - Paton Publ. House CY - Kiev ER - TY - CHAP A1 - Reindl, Lukas A1 - Butenweg, Christoph A1 - Kubalski, Thomas T1 - Numerical simulation of unreinforced masonry walls subject to dynamic out-of-plane loading T2 - COMPDYN 2011 : ECCOMAS Thematic Conference ; Proceedings of the 3rd International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering ; 25-28 May, 2011, Corfu, Greece / Eds.: M. Papadrakakis ... Y1 - 2011 SN - 978-960-99994-0-3 SP - 1 EP - 10 PB - National Technical Univ. of Athens CY - Athen ER - TY - CHAP A1 - Pfaff, Raphael A1 - Larkowski, Tomasz A1 - Burnham, Keith J. T1 - An application of adaptive control in the behavioural framework T2 - 21st International Conference on Systems Engineering (ICSEng) : 16 - 18 Aug. 2011, Las Vegas, Nevada ; proceedings Y1 - 2011 SN - 978-1-4577-1078-0 ; 978-0-7695-4495-3 SP - 49 EP - 54 PB - IEEE CY - Piscataway, NJ ER - TY - CHAP A1 - Park, Jin A1 - El-Daib, Khaled A1 - Butenweg, Christoph A1 - Gellert, Christoph T1 - A novel macroelement approach for masonry walls T2 - Proceedings of the 8th International Conference on Structural Dynamics, EURODYN 2011 : Leuven, Belgium, 4 - 6 July 2011 / Katholieke Universiteit Leuven, ... G. De Roeck ... (eds) Y1 - 2011 SN - 978-90-76019-31-4 SP - 3281 EP - 3286 PB - K. U. Leuven, Dep. of Civil Engineering CY - Leuven ER - TY - CHAP A1 - Olaru, Alexandra Maria A1 - Kowalski, Julia A1 - Sethi, Vaishali A1 - Blümich, Bernhard T1 - Fluid Transport in Porous Media probed by Relaxation-Exchange NMR T2 - 2011 Fall Meeting, AGU, San Francisco, Calif., 5-9 Dec. Y1 - 2011 N1 - H12B-07; American Geophysical Union ER - TY - CHAP A1 - Ohndorf, Andreas A1 - Dachwald, Bernd A1 - Seboldt, Wolfgang A1 - Schartner, Karl-Heinz T1 - Flight times to the heliopause using a combination of solar and radioisotope electric propulsion T2 - 32nd International Electric Propulsion Conference N2 - We investigate the interplanetary flight of a low-thrust space probe to the heliopause,located at a distance of about 200 AU from the Sun. Our goal was to reach this distance within the 25 years postulated by ESA for such a mission (which is less ambitious than the 15-year goal set by NASA). Contrary to solar sail concepts and combinations of allistic and electrically propelled flight legs, we have investigated whether the set flight time limit could also be kept with a combination of solar-electric propulsion and a second, RTG-powered upper stage. The used ion engine type was the RIT-22 for the first stage and the RIT-10 for the second stage. Trajectory optimization was carried out with the low-thrust optimization program InTrance, which implements the method of Evolutionary Neurocontrol,using Artificial Neural Networks for spacecraft steering and Evolutionary Algorithms to optimize the Neural Networks’ parameter set. Based on a parameter space study, in which the number of thrust units, the unit’s specific impulse, and the relative size of the solar power generator were varied, we have chosen one configuration as reference. The transfer time of this reference configuration was 29.6 years and the fastest one, which is technically more challenging, still required 28.3 years. As all flight times of this parameter study were longer than 25 years, we further shortened the transfer time by applying a launcher-provided hyperbolic excess energy up to 49 km2/s2. The resulting minimal flight time for the reference configuration was then 27.8 years. The following, more precise optimization to a launch with the European Ariane 5 ECA rocket reduced the transfer time to 27.5 years. This is the fastest mission design of our study that is flexible enough to allow a launch every year. The inclusion of a fly-by at Jupiter finally resulted in a flight time of 23.8 years,which is below the set transfer-time limit. However, compared to the 27.5-year transfer,this mission design has a significantly reduced launch window and mission flexibility if the escape direction is restricted to the heliosphere’s “nose". KW - low-thrust trajectory optimization KW - heliosphere KW - ion propulsion Y1 - 2011 N1 - IEPC-2011-051 32nd International Electric Propulsion Conference,September 11–15, 2011 Wiesbaden, Germany SP - 1 EP - 12 ER - TY - CHAP A1 - Meskouris, Konstantin A1 - Holtschoppen, Britta A1 - Butenweg, Christoph A1 - Rosin, Julia T1 - Seismic analysis of liquid storage tanks T2 - Earthquake Geology and Archaeology: Science, Society and Critical facilities : proceedings ; 2nd INQUA-IGCP 567 International Workshop on Active Tectonics, Earthquake Geology, Archaeology and Engineering ; 19-24 September 2011, Corinth (Greece) / Eds.: C. Grützner ; R. Pérez-Lopez ; T. Fernández Steeger ; I. Papanikolaou ; K. Reicherter ; P. G. Silva ; A. Vött. Volume 2 Y1 - 2011 SN - 978-960-466-093-3 SP - 136 EP - 139 PB - The Natural hazards Laboratory, National and Kapodistrian University of Athens CY - Athens ER - TY - CHAP A1 - Loeb, Horst W. A1 - Schartner, Karl-Heinz A1 - Dachwald, Bernd A1 - Ohndorf, Andreas A1 - Seboldt, Wolfgang T1 - An Interstellar – Heliopause mission using a combination of solar/radioisotope electric propulsion T2 - Presented at the 32nd International Electric Propulsion Conference N2 - There is common agreement within the scientific community that in order to understand our local galactic environment it will be necessary to send a spacecraft into the region beyond the solar wind termination shock. Considering distances of 200 AU for a new mission, one needs a spacecraft travelling at a speed of close to 10 AU/yr in order to keep the mission duration in the range of less than 25 yrs, a transfer time postulated by ESA.Two propulsion options for the mission have been proposed and discussed so far: the solar sail propulsion and the ballistic/radioisotope electric propulsion. As a further alternative, we here investigate a combination of solar-electric propulsion and radioisotope-electric propulsion. The solar-electric propulsion stage consists of six 22 cm diameter “RIT-22”ion thrusters working with a high specific impulse of 7377 s corresponding to a positive grid voltage of 5 kV. Solar power of 53 kW BOM is provided by a light-weight solar array. The REP-stage consists of four space-proven 10 cm diameter “RIT-10” ion thrusters that will be operating one after the other for 9 yrs in total. Four advanced radioisotope generators provide 648 W at BOM. The scientific instrument package is oriented at earlier studies. For its mass and electric power requirement 35 kg and 35 W are assessed, respectively. Optimized trajectory calculations, treated in a separate contribution, are based on our “InTrance” method.The program yields a burn out of the REP stage in a distance of 79.6 AU for a usage of 154 kg of Xe propellant. With a C3 = 45,1 (km/s)2 a heliocentric probe velocity of 10 AU/yr is reached at this distance, provided a close Jupiter gravity assist adds a velocity increment of 2.7 AU/yr. A transfer time of 23.8 yrs results for this scenario requiring about 450 kg Xe for the SEP stage, jettisoned at 3 AU. We interpret the SEP/REP propulsion as a competing alternative to solar sail and ballistic/REP propulsion. Omiting a Jupiter fly-by even allows more launch flexibility, leaving the mission duration in the range of the ESA specification. Y1 - 2011 N1 - 32nd International Electric Propulsion Conference, 11-15 September. Wiesbaden, Germany SP - 1 EP - 7 ER -