@masterthesis{Lenz2022,
  type      = {Bachelor Thesis},
  author    = {Lenz, Lena},
  title     = {Frauen sind der Boss : eine Kampagne f{\"u}r mehr Gleichberechtigung in F{\"u}hrungspositionen},
  publisher = {FH Aachen},
  address   = {Aachen},
  school      = {Fachhochschule Aachen},
  pages     = {93 Seiten},
  year      = {2022},
  abstract  = {Man k{\"o}nnte vermuten, dass in einem so weit entwickelten Land wie Deutschland Geschlechterdiskriminierung bereits erfolgreich {\"u}berwunden wurde - doch das entspricht nicht der Realit{\"a}t. Besonders in F{\"u}hrungspositionen f{\"a}llt dieses Ungleichgewicht auf. Eine Ursache daf{\"u}r ist das historisch etablierte Rollenverst{\"a}ndnis, aber auch vonseiten der Frauen gibt es h{\"a}ufig ein grundlegendes Problem: Sie trauen sich zu wenig zu. Die Kampagne soll junge Frauen dazu motivieren, ihre beruflichen Ambitionen hoch anzusetzen und zielstrebig zu verfolgen. Das Online-Portal "femiverse" ist dabei ihr Wegbereiter. Es erm{\"o}glicht einen direkten Austausch mit anderen Nutzer:innen und er{\"o}ffnet durch Workshops mit Unternehmer:innen neue Perspektiven. Die Bezeichnung „Powerfrau" ist {\"u}berholt - Frauen in F{\"u}hrungspositionen sind keine Ausnahmetalente, sie sind die Normalit{\"a}t von morgen.},
  language  = {de}
}
@article{HammerQuitterMayntzetal.2023,
  author    = {Hammer, Thorben and Quitter, Julius and Mayntz, Joscha and Bauschat, J.-Michael and Dahmann, Peter and G{\"o}tten, Falk and Hille, Sebastian and Stumpf, Eike},
  title     = {Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments},
  series = {CEAS Aeronautical Journal},
  journal   = {CEAS Aeronautical Journal},
  publisher = {Springer},
  address   = {Wien},
  issn      = {1869-5590 (Online)},
  doi       = {10.1007/s13272-023-00702-w},
  pages     = {14 Seiten},
  year      = {2023},
  abstract  = {New European Union (EU) regulations for UAS operations require an operational risk analysis, which includes an estimation of the potential danger of the UAS crashing. A key parameter for the potential ground risk is the kinetic impact energy of the UAS. The kinetic energy depends on the impact velocity of the UAS and, therefore, on the aerodynamic drag and the weight during free fall. Hence, estimating the impact energy of a UAS requires an accurate drag estimation of the UAS in that state. The paper at hand presents the aerodynamic drag estimation of small-scale multirotor UAS. Multirotor UAS of various sizes and configurations were analysed with a fully unsteady Reynolds-averaged Navier-Stokes approach. These simulations included different velocities and various fuselage pitch angles of the UAS. The results were compared against force measurements performed in a subsonic wind tunnel and provided good consistency. Furthermore, the influence of the UAS`s fuselage pitch angle as well as the influence of fixed and free spinning propellers on the aerodynamic drag was analysed. Free spinning propellers may increase the drag by up to 110\%, depending on the fuselage pitch angle. Increasing the fuselage pitch angle of the UAS lowers the drag by 40\% up to 85\%, depending on the UAS. The data presented in this paper allow for increased accuracy of ground risk assessments.},
  language  = {en}
}
@misc{RoesslerLeOtto2004,
  author    = {R{\"o}ßler, Edith and Le, Thi Lai and Otto, Moritz},
  title     = {Freilicht},
  year      = {2004},
  abstract  = {Eine kurze Folge einer Fernsehsendung namens "Freilicht", die Umweltprobleme und deren L{\"o}sungsm{\"o}glichkeiten in parodistischer Weise darstellt.},
  subject      = {Mediendesign},
  language  = {de}
}
@misc{OPUS4-10847,
  title     = {Fremdfirmenrichtlinie der FH Aachen},
  organization    = {FH Aachen},
  pages     = {17 Seiten},
  year      = {2019},
  language  = {de}
}
@masterthesis{Middelkoop2023,
  type      = {Bachelor Thesis},
  author    = {Middelkoop, Jonas},
  title     = {Frieden und Verschw{\"o}rung : ein kritischer Dokumentarfilm {\"u}ber Daniele Ganser},
  publisher = {FH Aachen},
  address   = {Aachen},
  school      = {Fachhochschule Aachen},
  pages     = {40 Seiten},
  year      = {2023},
  abstract  = {Im Umgang mit dem Schweizer Historiker Daniele Ganser l{\"a}sst sich ein ungew{\"o}hnliches Ph{\"a}nomen beobachten. W{\"a}hrend die Vortr{\"a}ge und B{\"u}cher des bekannten Publizisten bei zahlreichen Fans auf großes Interesse stoßen, zeichnen die meisten Medien das Bild eines gef{\"a}hrlichen Verschw{\"o}rungstheoretikers. Schnell wird seine Person zum Symbolbild einer ganzen Gegen{\"o}ffentlichkeit. Ein Dokumentarfilm {\"u}ber Daniele Ganser, seine Kritiker:innen und alternative Medien.},
  language  = {de}
}
@article{GoettenFingerHavermannetal.2021,
  author    = {G{\"o}tten, Falk and Finger, Felix and Havermann, Marc and Braun, Carsten and Marino, M. and Bil, C.},
  title     = {Full configuration drag estimation of short-to-medium range fixed-wing UAVs and its impact on initial sizing optimization},
  series = {CEAS Aeronautical Journal},
  volume    = {12},
  journal   = {CEAS Aeronautical Journal},
  publisher = {Springer},
  address   = {Berlin},
  issn      = {1869-5590 (Online)},
  doi       = {10.1007/s13272-021-00522-w},
  pages     = {589 -- 603},
  year      = {2021},
  abstract  = {The paper presents the derivation of a new equivalent skin friction coefficient for estimating the parasitic drag of short-to-medium range fixed-wing unmanned aircraft. The new coefficient is derived from an aerodynamic analysis of ten different unmanned aircraft used for surveillance, reconnaissance, and search and rescue missions. The aircraft is simulated using a validated unsteady Reynolds-averaged Navier Stokes approach. The UAV's parasitic drag is significantly influenced by the presence of miscellaneous components like fixed landing gears or electro-optical sensor turrets. These components are responsible for almost half of an unmanned aircraft's total parasitic drag. The new equivalent skin friction coefficient accounts for these effects and is significantly higher compared to other aircraft categories. It is used to initially size an unmanned aircraft for a typical reconnaissance mission. The improved parasitic drag estimation yields a much heavier unmanned aircraft when compared to the sizing results using available drag data of manned aircraft.},
  language  = {en}
}
@inproceedings{PoghossianSchumacherKloocketal.2006,
  author    = {Poghossian, Arshak and Schumacher, Kerstin and Kloock, Joachim P. and Rosenkranz, Christian and Schultze, Joachim W. and M{\"u}ller-Veggian, Mattea and Sch{\"o}ning, Michael Josef},
  title     = {Functional testing and characterisation of ISFETs on wafer level by means of a micro-droplet cell},
  url       = {http://nbn-resolving.de/urn:nbn:de:hbz:a96-opus-1259},
  year      = {2006},
  abstract  = {A wafer-level functionality testing and characterisation system for ISFETs (ionsensitive field-effect transistor) is realised by means of integration of a specifically designed capillary electrochemical micro-droplet cell into a commercial wafer prober-station. The developed system allows the identification and selection of "good" ISFETs at the earliest stage and to avoid expensive bonding, encapsulation and packaging processes for nonfunctioning ISFETs and thus, to decrease costs, which are wasted for bad dies. The developed system is also feasible for wafer-level characterisation of ISFETs in terms of sensitivity, hysteresis and response time. Additionally, the system might be also utilised for wafer-level testing of further electrochemical sensors.},
  subject      = {Biosensor},
  language  = {en}
}
@inproceedings{StaatBallmann1989,
  author    = {Staat, Manfred and Ballmann, J.},
  title     = {Fundamental aspects of numerical methods for the propagation of multi-dimensional nonlinear waves in solids},
  series = {Nonlinear hyperbolic equations : theory, computations methods, and applications ; proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen},
  booktitle = {Nonlinear hyperbolic equations : theory, computations methods, and applications ; proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen},
  pages     = {574 -- 588},
  year      = {1989},
  abstract  = {The nonlinear scalar constitutive equations of gases lead to a change in sound speed from point to point as would be found in linear inhomogeneous (and time dependent) media. The nonlinear tensor constitutive equations of solids introduce the additional local effect of solution dependent anisotropy. The speed of a wave passing through a point changes with propagation direction and its rays are inclined to the front. It is an open question whether the widely used operator splitting techniques achieve a dimensional splitting with physically reasonable results for these multi-dimensional problems. May be this is the main reason why the theoretical and numerical investigations of multi-dimensional wave propagation in nonlinear solids are so far behind gas dynamics. We hope to promote the subject a little by a discussion of some fundamental aspects of the solution of the equations of nonlinear elastodynamics. We use methods of characteristics because they only integrate mathematically exact equations which have a direct physical interpretation.},
  subject      = {Nichtlineare Welle},
  language  = {en}
}
@article{Wollert2014,
  author    = {Wollert, J{\"o}rg},
  title     = {Funkstandards f{\"u}r Sensornetzwerke},
  series = {Elektronik : Fachmedium f{\"u}r industrielle Anwender und Entwickler},
  volume    = {Bd. 63},
  journal   = {Elektronik : Fachmedium f{\"u}r industrielle Anwender und Entwickler},
  number    = {H. 12},
  publisher = {WEKA-Fachmedien},
  address   = {Haar},
  issn      = {0013-5658},
  pages     = {36 -- 41},
  year      = {2014},
  language  = {de}
}
@misc{Gebhardt2005,
  author    = {Gebhardt, Andreas},
  title     = {Fuzzy Regelung},
  year      = {2005},
  abstract  = {{\"U}berblick Fuzzy-Regler, Fuzzy Sets (Scharfe Mengen, Fuzzy Sets, Formen (st{\"u}ckweise linear, gaußf{\"o}rmig, glockenf{\"o}rmig), Eigenschaften (Gleichheit, Teilmenge)), Fuzzy Operatoren (NICHT, UND, ODER) Fuzzyfizierung Inferenzen (Verarbeitungsvorschrift, Ermittlung der aktiven Regeln, Ermittlung der Fuzzy Mengen, {\"U}berlagerung) Defuzzyfizierung (Mean-of-Maximum, Center-of-Gravity, Largest-of-Maximum, Smallest-of-Maximum, Center-of-Singletons) Entwurf, Beispiel, Fuzzy Tools, Internet, Literatur},
  language  = {de}
}