TY  - CHAP
A1  - Drumm, Christian
A1  - Lemcke, Jens
A1  - Oberle, Daniel
T1  - Business Process Management And Semantic Technologies
T2  - The Semantic Web
Y1  - 2007
SN  - 978-0-387-48531-7
U6  - https://doi.org/10.1007/978-0-387-48531-7_10
SP  - 207
EP  - 239
PB  - Springer
CY  - Boston, MA
ER  - 
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  - 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  - Weiss, Alexander
A1  - Abanteriba, Sylvester
A1  - Esch, Thomas
T1  - Investigation of Flow Separation Inside a Conical Rocket Nozzle With the Aid of an Annular Cross Flow
T2  - Proceedings of the ASME/JSME 2007 5th Joint Fluids Engineering Conference. Volume 1: Symposia, Parts A and B
N2  - Flow separation is a phenomenon that occurs in all kinds of supersonic nozzles sometimes during run-up and shut-down operations. Especially in expansion nozzles of rocket engines with large area ratio, flow separation can trigger strong side loads that can damage the structure of the nozzle. The investigation presented in this paper seeks to establish measures that may be applied to alter the point of flow separation. In order to achieve this, a supersonic nozzle was placed at the exit plane of the conical nozzle. This resulted in the generation of cross flow surrounding the core jet flow from the conical nozzle. Due to the entrainment of the gas stream from the conical nozzle the pressure in its exit plane was found to be lower than that of the ambient. A Cold gas instead of hot combustion gases was used as the working fluid. A mathematical simulation of the concept was validated by experiment. Measurements confirmed the simulation results that due to the introduction of a second nozzle the pressure in the separated region of the conical nozzle was significantly reduced. It was also established that the boundary layer separation inside the conical nozzle was delayed thus allowing an increased degree of overexpansion. The condition established by the pressure measurements was also demonstrated qualitatively using transparent nozzle configurations.
Y1  - 2007
SN  - 0-7918-4288-6
U6  - https://doi.org/10.1115/FEDSM2007-37387
N1  - Proceedings of the ASME/JSME 2007 5th Joint Fluids Engineering Conference. Volume 1: Symposia, Parts A and B. San Diego, California, USA. July 30–August 2, 2007
SP  - 1861
EP  - 1871
PB  - American Society of Mechanical Engineers (ASME)
CY  - New York
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  - 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  - 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  -