TY - THES A1 - Trzewik, Jürgen T1 - Experimental analysis of biaxial mechanical tension in cell monolayers and cultured three-dimensional tissues: the celldrum technology Y1 - 2007 N1 - Zugl.: Ilmenau, Techn. Univ., Diss., 2007 PB - Univeristätsverlg Ilmenau CY - Ilmenau ER - TY - JOUR A1 - Olbertz, Klaus T1 - Gleichstellungsabrede – Gestaltungsmöglichkeiten und -notwendigkeiten für die betriebliche Praxis JF - Betriebs-Berater: BB ; Recht, Wirtschaft, Steuern Y1 - 2018 SN - 0340-7918 N1 - gedruckt in der Bereichsbibliothek Eupener Str. unter der Signatur 43 Z 228 vorhanden SP - 2737 ER - TY - CHAP A1 - Barnat, Miriam T1 - Organisationale Lernprozesse und Machtquellen. Eine Fallstudie T2 - Beratung, Macht und organisationales Lernen Y1 - 2007 SN - 978-3-531-90752-9 U6 - https://doi.org/10.1007/978-3-531-90752-9_7 SP - 97 EP - 110 PB - VS Verlag für Sozialwissenschaften CY - Wiesbaden ER - TY - JOUR A1 - Waller, Mark P. A1 - Braun, Heiko A1 - Hojdis, Nils A1 - Bühl, Michael T1 - Geometries of Second-Row Transition-Metal Complexes from Density-Functional Theory JF - Journal of Chemical Theory and Computation Y1 - 2007 U6 - https://doi.org/10.1021/ct700178y SN - 1549-9626 VL - 3 IS - 6 SP - 2234 EP - 2242 ER - TY - JOUR A1 - Kroll-Ludwigs, Kathrin T1 - The Reform of German Maintenance Law JF - The International Survey of Family Law Y1 - 2018 SP - 85 EP - 100 ER - TY - CHAP A1 - Reimer, Lars A1 - Braun, Carsten A1 - Ballmann, Josef T1 - Computational study of the aeroelastic equilibrium configuration of a swept wind tunnel wing model in subsonic flow T2 - High performance computing in science and engineering '06. Transactions of the High Performance Computing Center Stuttgart (HLRS) 2006 / Wolfgang E. Nagel ... Eds. N2 - In the Collaborative Research Center SFB 401 at RWTH Aachen University, the numerical aeroelastic method SOFIA for direct numerical aeroelastic simulation is being progressively developed. Numerical results obtained by applying SOFIA were compared with measured data of static and dynamic aeroelastic wind tunnel tests for an elastic swept wing in subsonic flow. Y1 - 2007 SN - 978-3-540-36165-7 SP - 421 EP - 434 PB - Springer CY - Berlin [u.a.] ER - TY - JOUR A1 - Mistler, Michael A1 - Anthoine, A. A1 - Butenweg, Christoph T1 - In-plane and out-of-plane homogenisation of masonry JF - Computers & structures Y1 - 2007 U6 - https://doi.org/10.1016/j.compstruc.2006.08.087 SN - 1879-2243 (E-Journal); 0045-7949 (Print) VL - Volume 85 IS - Issues 17-18 SP - 1321 EP - 1330 ER - TY - JOUR A1 - Dachwald, Bernd A1 - Ohndorf, A. T1 - 1st ACT Global Trajectory Optimisation Competition : Results found at DLR JF - Acta Astronautica. 61 (2007), H. 9 Y1 - 2007 SN - 0094-5765 N1 - Global Trajectory Optimization ; Results of the First Competition Organised by the Advanced Concept Team (ACT) of the European Space Agency (ESA) SP - 742 EP - 752 ER - TY - CHAP A1 - Butenweg, Christoph T1 - Nachweis der Erdbebensicherheit von Silos aus Stahl unter Erdbebenbelastung T2 - D-A-CH Tagung 2007 : Aktuelle Themen des Erdbebeningenieurwesens und der Baudynamik ; 27. und 28. September 2007, arsenal research, TECHbase Vienna Y1 - 2007 SP - 1 EP - 14 ER - TY - JOUR A1 - Gömmel, Andreas A1 - Butenweg, Christoph A1 - Bolender, Katrin A1 - Grunendahl, Arno T1 - A muscle controlled finite-element model of laryngeal abduction and adduction JF - Computer methods in biomechanics and biomedical engineering Y1 - 2007 SN - 1476-8259 (E-Journal); 1025-5842 (Print) VL - Volume 10 IS - Issue 5 SP - 377 EP - 388 ER - TY - JOUR A1 - Butenweg, Christoph A1 - Gellert, Christoph A1 - Meskouris, Konstantin T1 - Mauerwerkswände unter zyklischer Schubbeanspruchung JF - Mauerwerk : European journal of masonry Y1 - 2007 U6 - https://doi.org/10.1002/dama.200700356 SN - 1437-1022 (E-Journal); 1432-3427 (Print) VL - Volume 11 IS - Issue 6 SP - 356 EP - 362 ER - TY - BOOK A1 - Meskouris, Konstantin A1 - Renault, Philippe A1 - Butenweg, Christoph A1 - Hinzen, Klaus-G. A1 - Weber, Bernd T1 - Gefährdungsabschätzung von Brücken in Deutschland unter Erdbebenbelastung. [Bericht zum Forschungs- und Entwicklungsvorhaben FE 15.393/2003/FRB des Bundesministeriums für Verkehr, Bau und Stadtentwicklung.] (Forschung Straßenbau und Straßenverkehrstechnik ; 952) Y1 - 2007 SN - 978-3-86509-602-9 PB - Bundesministerium für Verkehr, Bau und Stadtentwicklung, Abt. Straßenbau, Straßenverkehr CY - Bonn ER - TY - CHAP A1 - Meskouris, Konstantin A1 - Butenweg, Christoph A1 - Kalker, Ines A1 - Mistler, Michael T1 - Numerical simulation of historic masonry buildings T2 - Antike Erdbeben im alpinen und zirkumalpinen Raum : Befunde und Probleme in archäologischer, historischer und seismologischer Sicht ; Beiträge des Interdisziplinären Workshops Schloss Hohenkammer, 14./15. Mai 2004 = Earthquakes in antiquity in the alpine and circum-alpine region / Gerhard H. Waldherr ; Anselm Smolka (Hrsg.) (Geographica Historica ; 24) Y1 - 2007 SN - 978-3-515-09030-8 ; 3-515-09030-4 SP - 171 EP - 189 PB - Franz Steiner Verlag CY - Stuttgart ER - TY - CHAP A1 - Butenweg, Christoph A1 - Gellert, Christoph T1 - Berechnung und Bemessung von durch Erdbeben beanspruchten Mauerwerksbauten nach DIN 4149 (04.2005) T2 - Mauerwerksbau-Praxis / Schubert ; Schneider ; Schoch (Hrsg.) Y1 - 2007 SN - 3-9343-6938-3 ; 978-3-9343-6938-2 SP - 363 EP - 393 PB - Werner Verlag CY - Berlin ER - TY - BOOK A1 - Meskouris, Konstantin A1 - Hinzen, Klaus-Günter A1 - Butenweg, Christoph A1 - Mistler, Michael T1 - Bauwerke und Erdbeben : Grundlagen - Anwendung - Beispiele Y1 - 2007 SN - 3-8348-0146-1 ; 978-3-8348-0146-3 N1 - gedruckt in der Bereichsbibliothek Bayernallee unter der Signatur 11 XBM 41(2) vorhanden PB - Vieweg CY - Wiesbaden ET - 2., erweiterte und aktualisierte Auflage ER - TY - JOUR A1 - Zerlin, Kay A1 - Digel, Ilya A1 - Stadler, Andreas M. A1 - Büldt, Georg A1 - Zaccai, Guiseppe A1 - Artmann, Gerhard T1 - Dynamics and interactions of hemoglobin in human red blood cells and concentrated hemoglobin solutions JF - Regenerative medicine. 2 (2007), H. 5 Y1 - 2007 SN - 1746-0751 N1 - Proceedings of the 3rd World Congress on Regenerative Medicine. October 18-20, 2007. Leipzig, Germany SP - 573 EP - 573 ER - TY - JOUR A1 - Artmann, Gerhard A1 - Zerlin, Kay A1 - Digel, Ilya A1 - Stadler, Andreas M. T1 - Physical discontinuities at body temperature in human red blood cells / Artmann, GM ; Zerlin, K ; Digel, I ; Stadler, A ; Zaccai, G ; Temiz, AA JF - Tissue Engineering. 13 (2007), H. 7 Y1 - 2007 SN - 1076-3279 N1 - TERMIS-EU Meeting Abstracts London, UK September 4–7, 2007 SP - 1778 EP - 1778 ER - TY - CHAP A1 - Dachwald, Bernd A1 - Seboldt, Wolfgang A1 - Loeb, Horst W. A1 - Schartner, Karl-Heinz T1 - A comparison of SEP and NEP for a main belt asteroid sample return mission T2 - 7th International Symposium on Launcher Technologies, Barcelona, Spain, 02-05 April 2007 N2 - Innovative interplanetary deep space missions, like a main belt asteroid sample return mission, require ever larger velocity increments (∆V s) and thus ever more demanding propulsion capabilities. Providing much larger exhaust velocities than chemical high-thrust systems, electric low-thrust space-propulsion systems can significantly enhance or even enable such high-energy missions. In 1995, a European-Russian Joint Study Group (JSG) presented a study report on “Advanced Interplanetary Missions Using Nuclear-Electric Propulsion” (NEP). One of the investigated reference missions was a sample return (SR) from the main belt asteroid (19) Fortuna. The envisaged nuclear power plant, Topaz-25, however, could not be realized and also the worldwide developments in space reactor hardware stalled. In this paper, we investigate, whether such a mission is also feasible using a solar electric propulsion (SEP) system and compare our SEP results to corresponding NEP results. Y1 - 2007 SP - 1 EP - 10 ER - TY - CHAP A1 - Dachwald, Bernd A1 - Kahle, Ralph A1 - Wie, Bong T1 - Head-on impact deflection of NEAs: a case study for 99942 Apophis T2 - Planetary Defense Conference 2007 N2 - Near-Earth asteroid (NEA) 99942 Apophis provides a typical example for the evolution of asteroid orbits that lead to Earth-impacts after a close Earth-encounter that results in a resonant return. Apophis will have a close Earth-encounter in 2029 with potential very close subsequent Earth-encounters (or even an impact) in 2036 or later, depending on whether it passes through one of several less than 1 km-sized gravitational keyholes during its 2029-encounter. A pre-2029 kinetic impact is a very favorable option to nudge the asteroid out of a keyhole. The highest impact velocity and thus deflection can be achieved from a trajectory that is retrograde to Apophis orbit. With a chemical or electric propulsion system, however, many gravity assists and thus a long time is required to achieve this. We show in this paper that the solar sail might be the better propulsion system for such a mission: a solar sail Kinetic Energy Impactor (KEI) spacecraft could impact Apophis from a retrograde trajectory with a very high relative velocity (75-80 km/s) during one of its perihelion passages. The spacecraft consists of a 160 m × 160 m, 168 kg solar sail assembly and a 150 kg impactor. Although conventional spacecraft can also achieve the required minimum deflection of 1 km for this approx. 320 m-sized object from a prograde trajectory, our solar sail KEI concept also allows the deflection of larger objects. For a launch in 2020, we also show that, even after Apophis has flown through one of the gravitational keyholes in 2029, the solar sail KEI concept is still feasible to prevent Apophis from impacting the Earth, but many KEIs would be required for consecutive impacts to increase the total Earth-miss distance to a safe value Y1 - 2007 N1 - Planetary Defense Conference 2007, Wahington D.C., USA, 05-08 March 2007 SP - 1 EP - 12 ER - TY - CHAP A1 - Dachwald, Bernd T1 - Low-Thrust Mission Analysis and Global Trajectory Optimization Using Evolutionary Neurocontrol: New Results T2 - European Workshop on Space Mission Analysis ESA/ESOC, Darmstadt, Germany 10 { 12 Dec 2007 N2 - Interplanetary trajectories for low-thrust spacecraft are often characterized by multiple revolutions around the sun. Unfortunately, the convergence of traditional trajectory optimizers that are based on numerical optimal control methods depends strongly on an adequate initial guess for the control function (if a direct method is used) or for the starting values of the adjoint vector (if an indirect method is used). Especially when many revolutions around the sun are re- quired, trajectory optimization becomes a very difficult and time-consuming task that involves a lot of experience and expert knowledge in astrodynamics and optimal control theory, because an adequate initial guess is extremely hard to find. Evolutionary neurocontrol (ENC) was proposed as a smart method for low-thrust trajectory optimization that fuses artificial neural networks and evolutionary algorithms to so-called evolutionary neurocontrollers (ENCs) [1]. Inspired by natural archetypes, ENC attacks the trajectoryoptimization problem from the perspective of artificial intelligence and machine learning, a perspective that is quite different from that of optimal control theory. Within the context of ENC, a trajectory is regarded as the result of a spacecraft steering strategy that maps permanently the actual spacecraft state and the actual target state onto the actual spacecraft control vector. This way, the problem of searching the optimal spacecraft trajectory is equivalent to the problem of searching (or "learning") the optimal spacecraft steering strategy. An artificial neural network is used to implement such a spacecraft steering strategy. It can be regarded as a parameterized function (the network function) that is defined by the internal network parameters. Therefore, each distinct set of network parameters defines a different network function and thus a different steering strategy. The problem of searching the optimal steering strategy is now equivalent to the problem of searching the optimal set of network parameters. Evolutionary algorithms that work on a population of (artificial) chromosomes are used to find the optimal network parameters, because the parameters can be easily mapped onto a chromosome. The trajectory optimization problem is solved when the optimal chromosome is found. A comparison of solar sail trajectories that have been published by others [2, 3, 4, 5] with ENC-trajectories has shown that ENCs can be successfully applied for near-globally optimal spacecraft control [1, 6] and that they are able to find trajectories that are closer to the (unknown) global optimum, because they explore the trajectory search space more exhaustively than a human expert can do. The obtained trajectories are fairly accurate with respect to the terminal constraint. If a more accurate trajectory is required, the ENC-solution can be used as an initial guess for a local trajectory optimization method. Using ENC, low-thrust trajectories can be optimized without an initial guess and without expert attendance. Here, new results for nuclear electric spacecraft and for solar sail spacecraft are presented and it will be shown that ENCs find very good trajectories even for very difficult problems. Trajectory optimization results are presented for 1. NASA's Solar Polar Imager Mission, a mission to attain a highly inclined close solar orbit with a solar sail [7] 2. a mission to de ect asteroid Apophis with a solar sail from a retrograde orbit with a very-high velocity impact [8, 9] 3. JPL's \2nd Global Trajectory Optimization Competition", a grand tour to visit four asteroids from different classes with a NEP spacecraft Y1 - 2007 ER -