TY - CHAP A1 - Gonsior, Daniel A1 - Hoffschmidt, Bernhard T1 - Innovative Rußfilter für LKW-Dieselmotoren (Innotrap) T2 - Feinstaubforschung in Nordrhein-Westfalen. LANUV-Fachbericht. 9 Y1 - 2008 SN - 1864-3930 SP - 13 EP - 14 PB - Landesamt für Natur, Umwelt und Verbraucherschutz Nordrhein-Westfalen CY - Recklinghausen ER - TY - CHAP A1 - Kroker, Jan A1 - Hoffschmidt, Bernhard A1 - Schwarzer, Klemens A1 - Späte, Frank T1 - PTC 1000 modular parabolic trough collector T2 - Process heat collectors : state of the art within task 33/IV ; IEA SHC-Task 33 and SolarPACES-Task IV: Solar heat for industrial processes : Förderkennzeichen BMBF 0329273A / Solar Heating and Cooling Executive Committee of the International Energy Agency (IEA) ; ed. Werner Weiss Y1 - 2008 SP - 45 EP - 46 PB - AEE INTEC CY - Gleisdorf 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 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 - https://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 - 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 - CHAP A1 - Laack, Walter van ED - Beer, André-Michael ED - Adler, Martin T1 - Elektro- und Ultraschalltherapie T2 - Leitfaden Naturheilverfahren : für die ärztliche Praxis Y1 - 2012 SN - 978-3-437-56103-0 U6 - https://doi.org/10.1016/B978-3-437-56103-0.10013-5 SP - 285 EP - 299 PB - Elsevier CY - Amsterdam ER - TY - CHAP A1 - Hüning, Felix ED - Schmitz, Günter T1 - PowerMOSFETs für Elektromotoren im Automobil : Vom Fensterheber zum EPS T2 - Elektronik im Kraftfahrzeug : Innovationen bei Systemen und Komponenten ; mit 7 Tabellen Y1 - 2012 SN - 978-3-8169-3110-2 N1 - Haus der Technik Fachbuchreihe ; 123 SP - 71 EP - 81 PB - Expert Verlag CY - Renningen ER - TY - CHAP A1 - Wolf, Martin A1 - Fräntz, Birgit T1 - Erfolgreiches IT-Marketing T2 - Erfolgreiches IT-Marketing in Zeiten von Social Media, Cloud & Co. - (CIO-Handbuch ; 2) KW - IT-Marketing Y1 - 2013 SN - 978-3-86329-612-4 SP - 123 EP - 140 PB - Symposion Publishing CY - Düsseldorf ET - 1. Auflage ER - TY - CHAP A1 - Dören, Horst-Peter ED - Gümpel, Paul T1 - Schweißtechnische Verarbeitung nichtrostender Stähle T2 - Rostfreie Stähle. Grundwissen, Konstruktions- und Verarbeitungshinweise Y1 - 2008 SN - 978-3-8169-2689-4 SP - 140 EP - 174 PB - Expert Verlag CY - Renningen ER - TY - CHAP A1 - Buxbaum, Bernd A1 - Lange, Robert A1 - Ringbeck, Thorsten ED - Winner, Hermann T1 - 3D-Imaging T2 - Handbuch Fahrerassistenzsysteme : Grundlagen, Komponenten und Systeme für aktive Sicherheit und Komfort ; mit 45 Tabellen Y1 - 2009 SN - 978-3-8348-0287-3 SP - 187 EP - 197 PB - Vieweg + Teubner CY - Wiesbaden ET - 1. Auflage ER - TY - CHAP A1 - Funke, Harald A1 - Börner, Sebastian A1 - Hendrick, P. A1 - Recker, E. T1 - Modification and testing of an engine and fuel control system for a hydrogen fuelled gas turbine T2 - Progress in Propulsion Physics. Vol. 2 Y1 - 2011 SN - 978-2-7598-0673-7 SP - 475 EP - 486 PB - EDP Sciences CY - Les Ulis ER - TY - CHAP A1 - Ringbeck, Thorsten A1 - Hagebeuker, Bianca A1 - Kraft, Holger A1 - Paintner, Michael ED - Tille, Thomas T1 - PMD-basierte 3D-Optosensoren zur Fahrzeugumfelderfassung T2 - Sensoren im Automobil II : mit 27 Tabellen / [2. Tagung Sensoren im Automobil 2007] Y1 - 2007 SN - 978-3-8169-2750-1 N1 - Tagung Sensoren im Automobil <2, 2007, München> N1 - (Fachbuch ; Bd. 86) PB - expert-Verl. CY - Renningen ER - TY - CHAP A1 - Dören, Horst-Peter T1 - Nichtrostende Stähle T2 - Jahrbuch Schweißtechnik. 1988 Y1 - 1987 SN - 0935-0292 SP - 188 EP - 203 PB - Dt. Verl. für Schweißtechnik (DVS) CY - Düsseldorf ER - TY - CHAP A1 - Dören, Horst-Peter T1 - Das Schweißen von Austenit-Ferrit-Verbindungen T2 - Jahrbuch Schweißtechnik. 1991 Y1 - 1990 SN - 3-87155-725-0 SP - 57 EP - 63 PB - DVS-Verlag CY - Düsseldorf ER - TY - CHAP A1 - Schwarte, Rudolf A1 - Heinol, Horst-Guenther A1 - Buxbaum, Bernd A1 - Ringbeck, Thorsten A1 - [u.a.], ED - Jähne, Bernd T1 - Principles of three-dimensional imaging techniques T2 - Sensors and imaging. - (Handbook of computer vision and applications ; Vol. 1) Y1 - 1999 SN - 0-12-379771-3 (Einzelbd.) SN - 0-12-379770-5 (Gesamtwerk) SP - 463 EP - 485 PB - Academic Press CY - San Diego ER - TY - CHAP A1 - Claßen, R. A1 - Dören, Horst-Peter A1 - Codani, L. A1 - Watermeyer, Klaus T1 - Begleitende Untersuchungen beim Löten mit vorübergehend flüssiger Phase (TL PB) einschließlich Aktivkomponente an Verbindungen verschiedener Kupfer- und Kohlenstoffwerkstoffe (CFC). T2 - Fortschritte in der Metallographie. Vortragstexte der 33. Metallographie-Tagung, 15.-17. September 1999 in Rostock. Hrsg. Gerhard Schneider... Praktische Metallographie. Sonderband 31. Y1 - 2013 SP - 97 EP - 104 PB - Werkstoff-Informationsgesellschaft CY - Frankfurt ER -