TY - CHAP A1 - Schermutzki, Margret T1 - Learning outcomes - Lernergebnisse : Begriffe, Zusammenhänge, Umsetzung und Erfolgsermittlung. Lernergebnisse und Kompetenzvermittlung als elementare Orientierungen des Bologna-Prozesses N2 - Bei der Beschreibung der Studiengänge und Module durch die Hochschulen kommt der Ergebnisorientierung eine hohe Bedeutung zu. Der Beitrag beschreibt in diesem Zusammenhang zunächst die Vorgaben des europäischen Qualifikationsrahmens und der sich daraus ergebenden Fokussierung auf die Formulierung von Lernergebnissen. Der Schwerpunkt aber liegt auf praxisrelevanten Vorschlägen zu einem methodischen Vorgehen auf allen Ebenen von der Studiengangsbeschreibung über die Verteilung der Kompetenzarten über mehrere Module bis zur Wortwahl. Abschließend wird die an die Wahl der Lehr- und Lernformen geknüpfte Notwendigkeit der Veränderung der Prüfungsformen betont. Diese sollten inhaltlich und methodisch an die in den Studiengängen und Modulen beschriebenen Lernergebnisse und die Art der zu vermittelnden Kompetenzen angepasst werden. Vorabdruck des Aufsatzes. Erschienen in: Handbuch Qualität in Studium und Lehre : Evaluation nutzen, Akkreditierung sichern, Profil schärfen ( Hrsg. Winfried Benz ... . Berlin: Raabe Kapitel E 3.3 S. 1-30. ISBN 978-3-8183-0207-8 ; 3-8183-0207-3 1. Auflage des Aufsatzes unter dem Titel: Lernergebnisse - Begriffe, Zusammenhänge, Umsetzung und Erfolgsermittlung : Lernergebnisse und Kompetenzvermittlung als elementare Orientierungen des Bologna-Prozesses http://opus.bibliothek.fh-aachen.de/opus/volltexte/2007/232/ KW - Bologna-Prozess KW - Studiengangsentwicklung KW - Europäischer Qualifikationsrahmen KW - EQF KW - Lernergebnisorientierung Y1 - 2008 PB - FH Aachen ER - TY - CHAP A1 - Weßling, Matthias T1 - Plädoyer für eigenverantwortliches Lernen und Arbeiten im Hochschulstudium : Bedeutung und Folgerungen für Studierende und Lehrende T2 - Effektiver lernen - Zeit gewinnen N2 - Inhaltsverzeichnis: I. Lern- und Arbeitstechniken im 1. und im 10. Semester II. Lern- und Arbeitstechniken als persönliches Selbstmanagement III. Diskussionsfragen und -thesen IV. Was heißt: Eigenverantwortung im Studium? V. Eigenverantwortung als gelebte Freiheit von Studierenden VI. Warum es unmöglich ist, Verantwortung an Studierende zu delegieren VII. Erziehungsauftrag: Studierende in ihrer Eigenverantwortung belassen VIII. Folgerungen für Lehrende IX. Folgerungen für Studierende KW - Lernstil KW - Selbstorganisation KW - Effektives Lernen Y1 - 1997 SN - 3-87575-012-8 SP - 70 EP - 82 PB - Neinhaus CY - Stuttgart ER - TY - CHAP A1 - Fabo, Sabine ED - Brüstle, Christa T1 - Musik und Interaktivität : Modelle eines emanzipierten Handelns? T2 - Musik | Politik : Musik im Dialog (Jahrbuch der Berliner Gesellschaft für Neue Musik ; 5) Y1 - 2004 SN - 3-89727-257-1 VL - 2002 PB - Pfau Verlag CY - Saarbrücken ER - TY - CHAP A1 - Fabo, Sabine ED - Eming, Jutta T1 - Intermedia light : zur Erfüllung synästhetischer Phantasien in Echtzeit T2 - Mediale Performanzen : historische Konzepte und Perspektiven (Rombach Wissenschaften : Reihe Litterae ; 97) Y1 - 2002 SN - 3-7930-9344-1 SP - 197 EP - 220 PB - Rombach Verlag CY - Freiburg im Breisgau ER - TY - CHAP A1 - Fabo, Sabine ED - Köstler, Andreas ED - Hensel, Thomas T1 - Die Museumsinsel und die neuen Medien T2 - Einführung in die Kunstwissenschaft Y1 - 2004 SN - 3-496-01271-4 SP - 45 EP - 60 PB - Reimer CY - Berlin ER - TY - CHAP A1 - Lanzl, I. A1 - Seidova, S.-F. A1 - Dühring, C. von A1 - Kotliar, Konstantin ED - Erb, Carl T1 - Befunde der dynamischen Gefäßanalyse am Auge bei Gesunden und Glaukom-Patienten mit praxisrelevanter Bedeutung T2 - Mikrozirkulation beim Glaukom Y1 - 2009 N1 - Search on Glaucoma SP - 33 EP - 39 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Biener, Ernst T1 - Abfallwirtschaft T2 - Wendehorst Beispiele aus der Baupraxis / Otto W. Wetzell (Hrsg.). Bearb. von: Herwig Baumgartner ... Y1 - 2005 SN - 3-519-00489-5 N1 - Abschnitt 10 SP - 255 EP - 269 PB - Teubner CY - Stuttgart ER - TY - CHAP A1 - Biener, Ernst T1 - Abfallwirtschaft T2 - Bautechnische Zahlentafeln : mit 225 Beispielen / Wendehorst. Hrsg. von Otto W. Wetzell. Bearb. von Hubert Achten ... - 28., neubearb. Aufl. Y1 - 1998 SN - 3-519-25002-0 SP - 1265 EP - 1292 PB - Teubner [u.a.] CY - Stuttgart [u.a.] ER - TY - CHAP A1 - Staat, Manfred A1 - Heitzer, M. T1 - Basis reduction technique for limit and shakedown problems T2 - Numerical Methods for Limit and Shakedown Analysis. Deterministic and Probabilistic Approach. NIC Series Vol. 15 / Ed. by Staat, M.; Heitzer, M. Y1 - 2003 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:0001-2018112115 SN - 3-00-010001-6 SP - 1 EP - 55 PB - John von Neumann Institute for Computing (NIC) CY - Jülich ER - TY - CHAP A1 - Fabo, Sabine A1 - Eisenbeis, Manfred ED - Weber, Hermann T1 - Medienkultur : die mediale Konstruktion von Wirklichkeit T2 - Globalisierung der Zivilisation und überlieferte Kulturen : 28. - 30. April 1995 Y1 - 1995 SN - 3-926288-10-8 N1 - Jahresakademie / Katholischer Akademischer Ausländer-Dienst, KAAD ; [9] PB - Katholischer Akademischer Ausländer-Dienst CY - Bonn ER - TY - CHAP A1 - Fabo, Sabine ED - Hoffmann, Philipp T1 - Künstlerische Begegnungen zwischen Chaos und Kontrolle : Joyce, Beuys und Cage T2 - Chaos/control:complexity : chaos theory cultural production (Work - science - medium ; 1) Y1 - 2002 SN - 3-8258-6096-5 N1 - CD-ROM + Begleitheft (80 S.) PB - LIT Verlag CY - Hamburg ER - TY - CHAP A1 - Fabo, Sabine T1 - Ulysses in der Wärmezeitmaschine : Joseph Beuys liest James Joyce T2 - Joseph Beuys : Verbindungen im 20. Jahrhundert ; eine Tagung im Hessischen Landesmuseum Darmstadt, 5./6. Mai 2000 Y1 - 2001 SN - 3-926527-62-5 N1 - (Reihe XX. Jahrhundert) SP - 77 EP - 90 PB - Hessisches Landesmuseum CY - Darmstadt ER - TY - CHAP A1 - Fabo, Sabine ED - Krewani, Angela T1 - Born to be wired : Anmerkungen zur Sichtbarkeit von Netzwerken T2 - Artefakte Artefiktionen : Transformationsprozesse zeitgenössischer Literaturen, Medien, Künste, Architekturen für Christian W. Thomsen zum 60. Geburtstag Y1 - 2000 SN - 3-8253-1076-0 N1 - Parallelt.: Artefacts artefictions SP - 271 EP - 281 PB - Universitätsverlag Winter CY - Heidelberg ER - TY - CHAP A1 - Helsper, Christoph A1 - Fissan, H. J. A1 - Franzen, H. ED - Benarie, Michel M. T1 - Particle Size Distributions of Combustion Aerosols T2 - Atmospheric Pollution 1978 : Proceedings of the 13th International Colloquium; 25-28 April 1978; Paris, France; Edited by Michel M. Benarie N2 - It has been observed that carcinogenic polycyclic aromatic hydrocarbons (PAH) are present in the atmosphere. Combustion processes are considered the most important sources for PAH. Among these, the burning of coal produces the highest emission, but in cities with high traffic density and low meteorological exchange activities, vehicle emissions determine the immission situation, especially in narrow streets. For estimating the potential health effects caused by PAH, it is sufficient to characterize the emission of PAH with respect to their physical state, concentrations, and, as far as the particulate phase is concerned, size distribution. The size distribution is important for transport phenomena, inhalation, and deposition in the respiratory tract. These parameters mainly depend on the combustion system, on system operating conditions, on the exhaust system, and on exhaust cooling conditions. At exhaust-gas temperatures in the range of ambient air temperatures, almost the whole emission of PAH is made up of particulate matter. Y1 - 1978 SN - 0-444-41691-9 U6 - http://dx.doi.org/10.1016/S0166-1116(08)71583-8 SP - 263 EP - 266 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Mertens, Josef ED - Sobieczky, H. T1 - Aerodynamic multi point design challenge T2 - New design concepts for high speed air transport.- (Courses and lectures / International Centre for Mechanical Sciences ; 366) N2 - In the chapter “Son of Concorde, a Technology Challenge” one of the new challenges for a Supersonic Commercial Transport (SCT) is multi-point design for the four main design points: - supersonic cruise - transonic cruise - take-off and landing - transonic acceleration. KW - Drag Reduction KW - Pitching Moment KW - Leading Edge Vortex KW - Wave Drag KW - Variable Geometry Y1 - 1997 SN - 3-2118-2815-X U6 - http://dx.doi.org/10.1007/978-3-7091-2658-5_4 SP - 53 EP - 67 PB - Springer CY - Wien [u.a.] ER - TY - CHAP A1 - Mertens, Josef ED - Sobieczky, H. T1 - Required aerodynamic technologies T2 - New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366) N2 - In the preceeding chapters on “Son of Concorde, a Technology Challenge” and “Aerodynamic Multipoint Design Challenge” it was explained, that a well balanced contribution of new technologies in all major disciplines is required for realisation of a new Supersonic Commercial Transport (SCT). One of these technologies - usually one of the most important for aircraft-is aerodynamics. Here, the required “pure” aerodynamic technologies are specified in more detail, according to our present knowledge. Increasing insight into the problems may change the balance of importance of the individual technologies and may require some more contributions. We must never confine our knowledge to the knowledge base of an expert at a given time, but must stay open for new insights. KW - Mach Number KW - Wind Tunnel KW - Supersonic Flow KW - Pitching Moment KW - Wave Drag Y1 - 1997 SN - 3-2118-2815-X U6 - http://dx.doi.org/10.1007/978-3-7091-2658-5_5 SP - 69 EP - 96 PB - Springer CY - Wien [u.a.] ER - TY - CHAP A1 - Mertens, Josef ED - Sobieczky, H. T1 - Certification of supersonic civil transports T2 - New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366) N2 - Since certification of Concorde new certification standards were introduced including many new regulations to improve flight safety. Most of these standards are to prevent severe accidents in the future which happened in the past (here: after Concorde’s certification). A new SCT has to fulfill these standards, although Concorde had none of these accidents. But accidents - although they sometimes occurred only for a specific aircraft type - have to be avoided for any (new) aircraft. Because of existing aircraft without typical accident types having demonstrated their reliability, they are allowed to go on based on their old certification; although sometimes new rules prevent accident types which are not connected to specific aircraft types - like e.g. evacuation rules. Anyway, Concorde is allowed to fly based on its old certification, and hopefully in the future will fly as safely as in the past. But a new SCT has to fulfill updated rules like any other aircraft, and it has to be “just another aircraft” [75]. KW - Noise Exposure KW - Evacuation Rule KW - Severe Accident KW - Certification Rule KW - Thermal Fatigue Testing Y1 - 1997 SN - 3-2118-2815-X U6 - http://dx.doi.org/10.1007/978-3-7091-2658-5_6 SP - 97 EP - 103 PB - Springer CY - Wien [u.a.] ER - TY - CHAP A1 - Mertens, Josef ED - Sobieczky, H. T1 - Supersonic laminar flow T2 - New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366) N2 - Supersonic transports are very drag sensitive. Technology to reduce drag by application of laminar flow, therefore, will be important; it is a prerequisite to achieve very long range capability. In earlier studies it was assumed that SCTs would only become possible by application of laminar flow [376]. But today, we request an SCT to be viable without application of laminar flow in order to maintain its competitiveness when laminar flow becomes available for subsonic and supersonic transports. By reducing fuel burned, laminar flow drag reduction reduces size and weight of the aircraft, or increases range capability -whereas otherwise size and weight would grow towards infinity. Transition mechanisms from laminar to turbulent state of the boundary layer flow (ALT, CFI, TSI) function as for transonic transports, but at more severe conditions: higher sweep angles, cooled surfaces; higher mode instabilities (HMI) must at least be taken into account, although they may not become important below Mach 3. Hitherto there is a worldwide lack of ground test facilities to investigate TSI at the expected cruise Mach numbers between 1.6 and 2.4; in Stuttgart, Germany one such facility -a Ludwieg tube- is still in the validation phase. A quiet Ludwieg tunnel could be a favourable choice for Europe. But it will require a new approach in designing aircraft which includes improved theoretical predictions, usage of classical wind tunnels for turbulent flow and flight tests for validation. KW - Wind Tunnel KW - Flight Test KW - Supersonic Wind Tunnel KW - Parabolized Stability Equation Y1 - 1997 SN - 3-2118-2815-X U6 - http://dx.doi.org/10.1007/978-3-7091-2658-5_18 SP - 275 EP - 290 PB - Springer CY - Wien [u.a.] ER - TY - CHAP A1 - Mertens, Josef A1 - Becker, K. ED - Ballmann, Josef T1 - Numerical solution of flow equations : an aircraft designer's view T2 - Nonlinear hyperbolic equations - theory, computation methods, and applications : proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen, FRG, March 14 to 18, 1988. - (Notes on Numerical Fluid Mechanics ; 24) N2 - Today the most accurate and cost effective industrial codes used in aircraft design are based on the full potential equation coupled with boundary layer equations. However, these are not capable to solve complicated three-dimensional problems of vortical flows and shocks. On the other hand Euler and Navier-Stokes codes are too expensive and not accurate enough for design purposes, especially in regard of drag and interference prediction. The reasons for these deficiencies are investigated and a way to overcome them by future developments is demonstrated. Y1 - 1989 SN - 3-528-08098-1 U6 - http://dx.doi.org/10.1007/978-3-322-87869-4_41 N1 - International Conference on Nonlinear Hyperbolic Problems <3, 1988, Aachen> SP - 403 EP - 412 PB - Vieweg CY - Braunschweig ER - TY - CHAP A1 - Mertens, Josef ED - Sobieczky, H. T1 - Son of Concorde, a technology challenge T2 - New design concepts for high speed air transport. - (Courses and lectures / International Centre for Mechanical Sciences ; 366) N2 - Concorde (Figure 9) is the only supersonic airliner which has been introduced into regular passenger service. It is still in service at British Airways and Air France without any flight accidents, and probably will stay in service for at least for ten more years. KW - Technology Challenge KW - Multidisciplinary Design Optimization KW - Specific Fuel Consumption KW - Engine Efficiency KW - Sonic Boom Y1 - 1997 SN - 3-2118-2815-X U6 - http://dx.doi.org/10.1007/978-3-7091-2658-5_3 SP - 31 EP - 51 PB - Springer CY - Wien [u.a.] ER -