TY - CHAP A1 - Groß, Rolf Fritz A1 - Müller, D. A1 - Herting, D. A1 - Schneemann, A. A1 - Renz, Ulrich ED - Rahman, Jamal ED - Jaschinski, Hans T1 - Modulare Messdatenerfassung in Forschung und Lehre T2 - Virtuelle Instrumente in der Praxis : Begleitband zum Kongress VIP '97 N2 - The Lehrstuhl für Wärmeübertragung und Klimatechnik at the Aachen University of Technology operates several test facilities to investigate fundamentals of heat and mass transfer supported by the Deutsche Forschungsgemeinschaft, the Minister für Forschung und Technologie and the industry. In order to get high-resolution and reproselection of hardware components is as critical as the design of software routines to perform successful and accurate measurements. In the following the development of the measurement and control system for three different test facilities is presented and discussed. Special attention is given to the education of students within the framework of laboratories and scientific experiments. Y1 - 1997 SN - 978-3-7785-2667-5 Pp. SP - 282 EP - 288 PB - Hüthig CY - Heidelberg ER - TY - CHAP A1 - Borchert, Jörg T1 - Der Elektrizitätsmarkt in Indonesien und Beteiligungsmöglichkeiten privater Unternehmen T2 - Investitionsführer ASEAN, Indochina, 1997 : Brunei, Indonesien, Kambodscha, Laos, Malaysia, Myanmar, Philippinen, Singapur, Thailand, Vietnam Y1 - 2015 SP - 42 EP - 52 PB - Berliner Bank AG CY - Berlin ET - Stand: Mai 1997 ER - TY - CHAP A1 - Brandt, D. A1 - Güsken, J. A1 - Büchen, W. A1 - [u.a.], A1 - Wahle, Michael T1 - Konstruieren mit Aluminium [Kapitel 4] T2 - Aluminium-Taschenbuch / Hrsg.: Aluminium-Zentrale Düsseldorf. - Bd. 3: Weiterverarbeitung und Anwendung Y1 - 1997 SN - 3-87017-243-6 SP - 359 EP - 544 PB - Aluminium-Verlag CY - Düsseldorf ET - 15. Auflage ER - TY - CHAP A1 - Wahle, Michael ED - Reimerdes, Hans-G. T1 - Strukturmechanische Auslegung von Elastomer-Bauteilen in der Schwingungstechnik T2 - Kolloquium anläßlich des 70. Geburtstags von H. Öry : [29.09.1997 - 30.09.1997, Kármán-Auditorium, Hörsaal FO5, RWTH Aachen] Y1 - 1997 SP - 175 EP - 188 PB - Inst. für Leichtbau CY - Aachen ER - TY - CHAP A1 - Meliß, Michael A1 - Späte, Frank T1 - Auslegung von solarthermischen Anlagen T2 - Regenerative Energiequellen : Praktikum / ed. Michael Meliß Y1 - 1997 SN - 3-540-63218-2 U6 - http://dx.doi.org/10.1007/978-3-642-60864-3_3 SP - 23 EP - 47 PB - Springer CY - Berlin ER - TY - CHAP A1 - Meliß, Michael A1 - Späte, Frank T1 - Berechnung von Sonnenstand und -strahlung T2 - Regenerative Energiequellen : Praktikum / ed. Michael Meliß Y1 - 1997 SN - 3-540-63218-2 U6 - http://dx.doi.org/10.1007/978-3-642-60864-3_2 SP - 5 EP - 22 PB - Springer CY - Berlin ER - TY - CHAP A1 - Lincke, D.-M. A1 - Haertsch, P. A1 - Hoffmann, C. P. A1 - Lindemann, Markus T1 - Electronic Commerce Plattformen für den Werkzeugmaschinenbau T2 - Internet im Industriegütermarketing - Status quo und Entwicklungsperspektiven am Beispiel der Schweizer Werkzeugmaschinen-Industrie / Johannes Dickel ... (Hrsg.) Thexis-Fachbericht für Marketing. 97,4 Y1 - 1997 SN - 3-908545-38-2 SP - 60 EP - 85 PB - Thexis CY - St. Gallen ER - TY - CHAP A1 - Lindemann, Markus A1 - Klein, Stefan T1 - Die Nutzung von Internet-Diensten im Rahmen des Elektronischen Datenaustauschs - Architekturvarianten und ein Anwendungsszenario T2 - Wirtschaftsinformatik '97 - Internationale Geschäftstätigkeit auf der Basis flexibler Organisationsstrukturen und leistungsfähiger Informationssysteme / Hermann Krallmann (Hrsg.) Y1 - 1997 SN - 3-7908-0999-3 SP - 513 EP - 531 PB - Physica-Verlag CY - Heidelberg ER - TY - CHAP A1 - Mertens, Josef T1 - Reduction of aerodynamic drag (RaWid)-Status after the first year of the program T2 - New results in numerical and experimental fluid mechanics. - (Notes on numerical fluid mechanics ; 60) N2 - The technology programme “Reduction of aerodynamic drag (RaWid)” for high speed aerodynamics at Daimler-Benz Aerospace Airbus is sponsered by the German ministry for education, research and technology since July 1, 1995. Connected to this industrial programme are the cooperation programmes “MEGAFLOW” under leadership of the DLR and “Transition” by the DFG, and several contributions by DLR and universities. The programme is oriented towards technologies required for a MEGALINER which gains momentum by the ambitious plans for a new large Airbus A3XX. In the first year new technological steps were undertaken in theory, design and experiment. Some critical steps were verified by wing designs checked in wind tunnel tests. KW - Wind Tunnel KW - Aerodynamic Drag KW - Flight Test KW - Friction Drag Y1 - 1997 SN - 3-528-06960-0 U6 - http://dx.doi.org/10.1007/978-3-322-86573-1_2 SP - 7 EP - 14 PB - Vieweg CY - Braunschweig [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 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 - 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 - 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 -