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 - 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 - 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 - JOUR A1 - Pelikan, Erich A1 - Scholl, Ingrid T1 - Die Wavelet-Transformation. Pelikan, Erich; Scholl, Ingrid JF - Bildverarbeitung für die Medizin. Lehmann, T.; Oberschelp, W.; Pelikan, E.; Repges,R. Y1 - 1997 SP - 253 EP - 282 PB - Springer CY - Berlin 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 - 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 -