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 - JOUR A1 - Makovicka, C. A1 - Gärtner, G. A1 - Hardt, Arno A1 - Hermann, W. A1 - Wiechert, D. U. T1 - Impregnated cathode surface investigations by SFM/STM and SEM/EDX JF - Applied surface science. Vol. 111 Y1 - 1997 SN - 1873-5584 (E-Journal); 0169-4332 (Print) SP - 70 EP - 75 ER - TY - JOUR A1 - Mayer, Claudia T1 - L'Estétique et le pouvoir: Le discours chaotique de l'Allemagne unifiée JF - Canadian review of comparative literature : CRCL = Revue canadienne de littérature comparée : RCLC / Canadian Comparative Literature Association. 24 (1997), H. 2 Y1 - 1997 SN - 0319-051X SP - 297 EP - 317 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 - https://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 - https://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 - https://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 - 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 - https://doi.org/10.1007/978-3-7091-2658-5_3 SP - 31 EP - 51 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 - https://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 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 - https://doi.org/10.1007/978-3-322-86573-1_2 SP - 7 EP - 14 PB - Vieweg CY - Braunschweig [u.a.] ER - TY - JOUR A1 - Müller-Veggian, Mattea A1 - Colautti, P. A1 - Schröder, M. A1 - Tornielli, G. T1 - Electric field Gradient Effects in TEPS JF - Annual report / Istituto Nazionale di Fisica Nucleare, LNL, Laboratori Nazionali di Legnaro. 1996 (1997) Y1 - 1997 N1 - Nebent.: Annual Report LNL-INFN SP - 253 EP - 254 ER - TY - JOUR A1 - Reißel, Martin T1 - Three-dimensional eddy-current computation using Krylov subspace methods / Reissel, Martin JF - IMA Journal of Mathematics Applied in Business and Industry. 8 (1997), H. 2 Y1 - 1997 SN - 1471-678X SP - 99 EP - 121 ER - TY - JOUR A1 - Schelthoff, Christof A1 - Basermann, Achim A1 - Reichel, Björn T1 - Preconditioned CG methods for sparse matrices on massively parallel machines / Basermann, A. ; Reichel, B. ; Schelthoff, C. JF - Parallel Computing. 23 (1997), H. 3 Y1 - 1997 SN - 0167-8191 SP - 381 EP - 398 ER - TY - JOUR A1 - Scherer, Ulrich W. A1 - Hör, G. T1 - Artifacts and Pitfalls in FDG-PET Whole-Body Scans / U.W. Scherer, G. Hör JF - Radionuclides for Mammary Gland - Current Status and Future Aspects / G. S. Limouris [Hrsg.] Y1 - 1997 SN - 960-85227-6-5 SP - 37 EP - 42 PB - Mediterra Publishers CY - Athen ER - TY - JOUR A1 - Schmidt, Daniela A1 - Langen, Karl-J. A1 - Herzog, Hans A1 - Wirths, Jochen A1 - Holschbach, Markus A1 - Kiwit, Jürgen C. W. A1 - Ziemons, Karl A1 - Coenen, Heinz-H. A1 - Müller-Gärtner, Hans-W. T1 - Whole-body kinetics and dosimetry of L-3[123I]-iodo-α-methyltyrosine JF - European Journal of Nuclear Medicine Y1 - 1997 SN - 1619-7089 VL - 24 IS - 9 SP - 1162 EP - 1166 ER - TY - JOUR A1 - Schuba, Marko T1 - A Performance Evaluation of Connectionless Overlay Networks for ATM JF - INFOCOM ´97. Sixteenth Annual Joint Conference of the IEEE Computer and Communications Societies. Proceedings Vol. 1 Y1 - 1997 SN - 0-8186-7780-5 N1 - http://www.schuba.fh-aachen.de/papers/97-INFOCOM.pdf SP - 152 EP - 158 ER - TY - JOUR A1 - Schuba, Marko A1 - Reichl, Peter A1 - Hoff, Simon T1 - How to Model Complex Periodic Traffic with TES / Reichl, Peter ; Schuba, Marko ; Hoff, Simon JF - Proc. of 13th United Kingdom Workshop on Performance Engineering, Edinburgh, UK, July 1997 Y1 - 1997 SP - 17/1 EP - 17/11 ER - TY - JOUR A1 - Schäfer, Horst A1 - Worschech, L. A1 - Ossau, W. A1 - Fischer, C. T1 - Characterization of structural defects in MBE grown ZnSe JF - Materials Science and Engineering B. 43 (1997), H. 1-3 Y1 - 1997 SN - 0921-5107 N1 - Beitrag zum EMRS - Spring Meeting, 4.-7.06.1996 Strasbourg SP - 29 EP - 32 ER - TY - JOUR A1 - Schöning, Michael Josef A1 - Ronkel, F. A1 - Crott, M. A1 - Thust, M. (u.a.) T1 - Miniaturization of potentiometric sensors using porous silicon microtechnology JF - Electrochimica Acta. 42 (1997), H. 22 Y1 - 1997 SN - 0013-4686 SP - 3185 EP - 3193 ER - TY - JOUR A1 - Schöning, Michael Josef A1 - Schütz, S. A1 - Riemer, A. A1 - Weißbecker, B. A1 - Steffen, A. A1 - Kordos, P. A1 - Lüth, H. A1 - Hummel, Hans E. T1 - A BioFET on the basis of intact insect antennae JF - Proceedings of the 11th European Conference on Solid-State Transducers / Eurosensors XI, September 21 - 24, 1997, Warsaw, Poland. [Organised by] Warsaw University of Technology. Vol 2. Y1 - 1997 SN - 83-908335-0-6 N1 - Eurosensors ; (11, 1997, Warszawa) ; Eurosensors - European Conference on Solid-State Transducers ; (11 : ; 1997.09.21-24 : ; Warsaw) SP - 1461 EP - 1464 PB - Sensor Lab Sp. CY - Warsaw ER - TY - JOUR A1 - Schöning, Michael Josef A1 - Weidenbrück, B. A1 - Thust, M. A1 - Kordos, P. A1 - Lüth, H. T1 - A silicon-based sensor array with capacitive EIS structures JF - Proceedings of the 11th European Conference on Solid-State Transducers / Eurosensors XI, September 21 - 24, 1997, Warsaw, Poland. [Organised by] Warsaw University of Technology. Vol 2. Y1 - 1997 SN - 83-908335-0-6 N1 - Eurosensors ; (11, 1997, Warszawa) ; Eurosensors - European Conference on Solid-State Transducers ; (11 : ; 1997.09.21-24 : ; Warsaw) SP - 871 EP - 874 PB - Sensor Lab Sp. CY - Warsaw ER -