TY - BOOK A1 - Maercker, Gisela T1 - Statistical inference in conditional heteroskedastic autoregressive models Y1 - 1997 SN - 3-8265-2486-1 N1 - Berichte aus der Mathematik ; Zugl.: Braunschweig, Techn. Univ., Diss., 1996 PB - Shaker CY - Aachen ER - TY - BOOK A1 - Schwarzer, Klemens A1 - Meer, Andreas von A1 - Siggelkow, Patricio T1 - Entwicklung und Erprobung von kleinen regenerativen Energiesystemen für den ländlichen Raum in Chile : Schlußbericht ; gefördert durch den Bundesminister für Bildung und Technologie, Förderkennzeichen: 0329179 A/B ; Laufzeit: 01.07.1991 - 31.12.1995 / Andreas von Meer ; Klemens Schwarzer ; Patricio Siggelkow. - (Berichte aus der Energietechnik) Y1 - 1997 SN - 3-8265-2112-9 PB - Shaker CY - Aachen ER - TY - JOUR A1 - Thielemann, Frank A1 - Staudt, Erich T1 - Kompetenz zur Innovation: Vom Druckbetrieb zum Multimedia-Dienstleister . Staudt, E.; Thielemann, F. JF - News Letter (der Gesellschaft für Wirtschaftsförde­rung Duisburg) (1997) Y1 - 1997 SP - 3 EP - 3 ER - TY - JOUR A1 - Thielemann, Frank A1 - Staudt, Erich T1 - Reicht die Kompetenz zur Innovation? Staudt, E.; Thielemann, F. JF - OP DruckMagazin. 39 (1997), H. 10 Y1 - 1997 SN - 0030-0594 SP - 30 EP - 32 ER - TY - JOUR A1 - Thielemann, Frank T1 - Chancen durch Online-Dienste? JF - OP DruckMagazin. 39 (1997), H. 1-2 Y1 - 1997 SN - 0030-0594 SP - 26 EP - f. ER - TY - JOUR A1 - Temiz Artmann, Aysegül A1 - Baskurt, O. K. A1 - Meiselman, H. J. T1 - Red blood cell aggregation in experimental sepsis . Baskurt, O. K.; Temiz, A.; Meiselman, H. J. JF - Journal of Laboratory and Clinical Medicine. 130 (1997), H. 2 Y1 - 1997 SN - 0022-2143 SP - 183 EP - 190 ER - TY - JOUR A1 - Thielemann, Frank A1 - Staudt, Erich A1 - Kriegesmann, Bernd T1 - Neuformierung von Wertschöpfungsketten: Das Beispiel Druckindustrie . Staudt, Erich; Kriegesmann, Bernd; Thielemann, Frank JF - Zeitschrift Führung und Organisation. 96 (1997), H. 2 Y1 - 1997 SN - 0044-3212 N1 - in der Bereichsbibliothek Eupener Str. unter der Signatur 43 Z 367-1997 vorhanden SP - 75 EP - 80 ER - TY - JOUR A1 - Hillen, Walter A1 - Barry, J. C. A1 - Pongs, U. M. T1 - Algorithm for Purkinje Image I and IV and Limbus Centre Location. Barry, J. C.; Pongs, U. M.; Hillen, W. JF - Computers in Biology and Medicine. 27 (1997), H. 6 Y1 - 1997 SN - 0010-4825 SP - 515 EP - 531 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 - JOUR A1 - Scholl, Ingrid A1 - Kreutz, Reinhard A1 - Conradi, Helmut A1 - Spitzer, Klaus T1 - Orientierungs- und Benutzerunterstützung in Web-Dokumenten. Kreutz, Reinhard; Conradi, Helmut; Scholl, Ingrid; Spitzer, Klaus JF - Informatik '97 : Informatik als Innovationsmotor ; 27. Jahrestagung der Gesellschaft für Informatik Aachen, 24. - 26. September 1997 / Hrsg.: Matthias Jarke ... Y1 - 1997 SN - 3-540-63066-X SP - 516 EP - 517 PB - Springer CY - Berlin ER - TY - JOUR A1 - Scholl, Ingrid A1 - Kreutz, Reinhard A1 - Scholz, C. A1 - Conradi, H. T1 - Ein Modell zum Aufbau multimedialer medizinischer Lern- und Nachschlagedokumente. Kreutz, R.; Scholz, C.; Conradi, H.; Scholl, I.; Spitzer, K. JF - Medizinische Informatik, Biometrie und Epidemiologie : GMDS '97 ; Ulm, September 1997 / R. Muche ... (Hrsg.) Y1 - 1997 SN - 3-8208-1315-2 N1 - Jahrestagung der Deutschen Gesellschaft für Informatik, Biometrie und Epidemiologie (GMDS) ; 42 SP - 121 EP - 125 PB - MVV, Medizin-Verl. CY - München ER - TY - JOUR A1 - Scholl, Ingrid A1 - Sovakar, Abhijit A1 - Spitzer, Klaus T1 - Konturverfolgung der Stimmlippen in laryngoskopischen Bildsequenzen JF - Medizinische Informatik, Biometrie und Epidemiologie, GMDS '96, 41. Jahrestagung der GMDS, Bonn, September 1996 Y1 - 1997 SN - 3820812954 SP - 123 EP - 129 PB - MVV, Medizin-Verl. CY - München ER - TY - JOUR A1 - Scholl, Ingrid A1 - Conradi, Helmut A1 - Wirtz, D. A1 - Spreckelsen, Cord T1 - OrthoDocs - Ein modellbasiertes Werkzeug zur Erstellung orthopädischer Lerndokumente. Conradi, Helmar; Wirtz, D.; Spreckelsen, Cord; Scholl, Ingrid; Kreutz, Reinhard; Forst, R.; Spitzer, Klaus JF - Medizinische Informatik, Biometrie und Epidemiologie, GMDS '96, 41. Jahrestagung der GMDS, Bonn, September 1996 Y1 - 1997 SN - 3820812954 SP - 169 EP - 173 PB - MVV, Medizin-Verl. CY - München ER - TY - JOUR A1 - Scholl, Ingrid A1 - Palm, Christoph A1 - Lehmann, Thomas Martin A1 - Spitzer, Klaus T1 - Quantitative Analyse der Stimmlippen JF - 5. Workshop Digitale Bildverarbeitung in der Medizin : Freiburg, 10. -11. März 1997 / Universität Freiburg. [Bernhard Arnolds ... (Hrsg.)] Y1 - 1997 SN - 3-9805054-2-1 SP - 81 EP - 86 PB - Zentralstelle für Forschungsförderung und Technologietransfer CY - Freiburg 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 - JOUR A1 - Hoffschmidt, Bernhard A1 - Pitz-Paal, R. A1 - Böhmer, M. T1 - Experimental and numerical evaluation of the performance and flow stability of different types of open volumetric absorbers under non-homogeneous irradiation / R. Pitz-Pahl ; B. Hofschmidt ; M. Böhmer ... JF - Solar energy. 60 (1997), H. 3-4 Y1 - 1997 SN - 0038-092X SP - 135 EP - 150 ER - TY - BOOK A1 - Stulpe, Werner T1 - Classical Representations of Quantum Mechanics Related to Statistically Complete Observables Y1 - 1997 SN - 3-89685-438-0 N1 - Zugl. Berlin, Techn. Univ., Habil.-Schr. 1997 PB - Wissenschaft und Technik Verl. CY - Berlin ER -