TY - BOOK A1 - Benkö, Marietta A1 - Plescher, Engelbert T1 - Space law: reconsidering the definition/delimitation question and the passage of spacecraft through foreign airspace. (Essential air and space law ; 12) Y1 - 2013 SN - 9789462360761 ; 9462360766 ; 9789460948176 PB - Eleven International Publishing CY - The Hague ER - TY - JOUR A1 - Grundmann, Jan Thimo A1 - Dachwald, Bernd A1 - Grimm, Christian D. A1 - Kahle, Ralph A1 - Koch, Aaron Dexter A1 - Krause, Christian A1 - Lange, Caroline A1 - Quantius, Dominik A1 - Ulamec, Stephan T1 - Spacecraft for Hypervelocity Impact Research – An Overview of Capabilities, Constraints and the Challenges of Getting There JF - Procedia Engineering Y1 - 2015 U6 - https://doi.org/10.1016/j.proeng.2015.04.021 SN - 1877-7058 N1 - Proceedings of the 2015 Hypervelocity Impact Symposium (HVIS 2015) VL - Vol. 103 SP - 151 EP - 158 PB - Elsevier CY - Amsterdam ER - TY - JOUR A1 - Gazda, Quentin A1 - Maurischat, Andreas T1 - Special functions and Gauss-Thakur sums in higher rank and dimension Y1 - 2020 PB - De Gruyter CY - Berlin ER - TY - CHAP A1 - Dahmann, Peter T1 - Stemme S10 VTX als multifunktionales Forschungsflugzeug T2 - Deutscher Luft- und Raumfahrtkongress 2011 : Bremen, 27. bis 29. September 2011 ; Tagungsband Y1 - 2011 SN - 978-3-9321-8274-7 SP - 357 EP - 364 PB - Dt. Gesellschaft für Luft- und Raumfahrt CY - Bonn ER - TY - BOOK A1 - Blome, Hans-Joachim ED - Raith, Wilhelm T1 - Sterne und Weltraum Y1 - 2002 SN - 3-11-016866-9 N1 - Lehrbuch der Experimentalphysik ; 8 PB - de Gruyter CY - Berlin [u.a.] ET - 2., stark erw. und aktualisierte Aufl. ER - TY - JOUR A1 - Blome, Hans-Joachim T1 - Sternstunden der Astronomie Extraterrestrische Grundlagenforschung JF - Kultur und Technik. 23 (1999), H. 1 Y1 - 1999 SN - 0344-5690 SP - 18 EP - 27 ER - TY - JOUR A1 - Gerhardt, Hans Joachim A1 - Rudolph, M. T1 - Steuerungsstrategien für Fensterbetätigungen von Hochhäusern. Natürliche Lüftung JF - HLH - Heizung, Lüftung, Klima, Haustechnik. 51 (2000), H. 9 Y1 - 2000 SN - 1436-5103 SP - 48 EP - 52 ER - TY - PAT A1 - Wahle, Michael T1 - Stoßdämpfer : Offenlegungschrift / Europäische Patentschrift T1 - Shock absorber : patent of invention Y1 - 1994 PB - Deutsches Patent- und Markenamt / Europäisches Patentamt CY - München / Den Hague ER - TY - BOOK A1 - Havermann, Marc T1 - Strahlmischung und Druckrückgewinn in Überschall-Innenströmungen Y1 - 2000 SN - 3-86073-761-9 N1 - Aachener Beiträge zum Maschinenbau ; 2 ; Zugl. Aachen, Techn. Hochsch., Diss., 1999 PB - Mainz CY - Aachen ER - TY - CHAP A1 - Kapoor, Hrshi A1 - Boller, Christian A1 - Giljohann, Sebastian A1 - Braun, Carsten T1 - Strategies for structural health monitoring implementation potential assessment in aircraft operational life extension considerations T2 - 2nd International Symposium on NDT in Aerospace : November 22-24, 2010 Hamburg, Germany Y1 - 2010 SN - 978-3-940283-28-3 PB - Dt. Gesellschaft für Zerstörungsfreie Prüfung CY - Berlin ER - TY - RPRT A1 - Barnat, Miriam A1 - Arntz, Kristian A1 - Bernecker, Andreas A1 - Fissabre, Anke A1 - Franken, Norbert A1 - Goldbach, Daniel A1 - Hüning, Felix A1 - Jörissen, Jörg A1 - Kirsch, Ansgar A1 - Pettrak, Jürgen A1 - Rexforth, Matthias A1 - Josef, Rosenkranz A1 - Terstegge, Andreas T1 - Strategische Gestaltung von Studiengängen für die Zukunft: Ein kollaborativ entwickeltes Self-Assessment BT - Diskussionspapier Nr. 33 T2 - Hochschulforum Digitalisierung - Diskussionspapier N2 - Das Diskussionspapier beschreibt einen Prozess an der FH Aachen zur Entwicklung und Implementierung eines Self-Assessment-Tools für Studiengänge. Dieser Prozess zielte darauf ab, die Relevanz der Themen Digitalisierung, Internationalisierung und Nachhaltigkeit in Studiengängen zu stärken. Durch Workshops und kollaborative Entwicklung mit Studiendekan:innen entstand ein Fragebogen, der zur Reflexion und strategischen Weiterentwicklung der Studiengänge dient. Y1 - 2024 SN - 2365-7081 PB - Stifterverband für die Deutsche Wissenschaft CY - Berlin ER - TY - THES A1 - Kowalski, Julia T1 - Streamline estimation from sparsely sampled q-space Magnetic Resonance data Y1 - 2010 N1 - Master Thesis in Medical Physics, ETH Zurich ER - TY - GEN A1 - Machado, Patricia Almeida A1 - Dahmann, Peter A1 - Keimer, Jona A1 - Saretzki, Charlotte A1 - Stübing, Felix A1 - Küpper, Thomas T1 - Stress profile and individual workload monitoring in general aviation pilots – an experiment’s setting T2 - 23. Annual Meeting of the German Society of Travel Medicine, Coburg, 18.-19.9.2020 Y1 - 2020 U6 - https://doi.org/10.55225/hppa.156 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 - BOOK A1 - Janser, Frank A1 - Havermann, Marc A1 - Hoeveler, Bastian A1 - Hertz, Cyril A1 - Bergmann, Ole T1 - Strömungslehre und Aerodynamik : inkompressible Profile und Tragflügelaerodynamik, Band 2 N2 - Das vorliegende Buch dient als Grundlage für die Bachelor- und Master-Ausbildung von Studierenden im Fachgebiet Strömungslehre und Aerodynamik. Im hier behandelten Teilbereich der inkompressiblen Profile und Tragflügelaerodynamik werden schwerpunktmäßig die folgenden Themen besprochen: - Profilaerodynamik - Tragflügelaerodynamik - Flugzeugpolare - Methoden zur Flugbereichserweiterung - Schwebeschub und Schwebeleistung - Propellerblattaerodynamik - Numerische Methoden zur Tragflügelberechnung Y1 - 2023 SN - 978-3-8107-0261-6 PB - Mainz CY - Aachen ET - 4. Auflage ER - TY - JOUR A1 - Matheis, Anton A1 - Röth, Thilo A1 - Wagner, Manfred T1 - Studentenprojekt "Capro" – eine virtuelle Sportwagenstudie "Vision 2015" N2 - Design- und Karosseriebaustudenten der FH Aachen entwickeln gemeinsam mit externen Fachleuten unter Einsatz virtueller Entwicklungswerkzeuge ein Konzept für einen Sportwagen KW - Karosseriebau KW - Sportwagen KW - Kraftfahrzeugbau KW - Studentenprojekt KW - Virtuelle Fahrzeugentwicklung KW - car body construction Y1 - 2005 ER - TY - JOUR A1 - Henn, Gudrun A1 - Polaczek, Christa T1 - Studienerfolg in den Ingenieurwissenschaften JF - Das Hochschulwesen : HSW ; Forum für Hochschulforschung, -praxis und -politik Y1 - 2007 SN - 0018-2974 VL - 55 IS - 5 SP - 144 EP - 147 ER - TY - BOOK A1 - Havermann, Marc A1 - Seiler, F. A1 - Gnemmi, P. A1 - Ende, H. T1 - Study on lateral jet/cross flow interaction in the High Energy ISL Shock Tunnel : 23rd International Symposium on Shock Waves, Fort Worth/TX, USA, July 22 - 27, 2001 / Institut Franco-Allemand de Recherches de Saint-Louis. Seiler, F. ; Gnemmi, P. ; Ende, H. ; Havermann, M. ; Schwenzer, M.... Y1 - 2001 PB - ISL CY - Saint-Louis ER - TY - CHAP A1 - Bergmann, Kevin A1 - Gräbener, Josefine A1 - Wild, Dominik A1 - Ulfers, H. A1 - Czupalla, Markus T1 - Study on thermal stabilization of a GEO-stationary telescope baffling system by integral application of phase change material T2 - International Conference on Environmental Systems N2 - The utilization of phase change material (PCM) for latent heat storage and thermal control of spacecraft has been demonstrated in the past in few missions only. One limiting factor was the fact that all concepts developed so far envisioned the PCM to be applied as an additional capacitor, encapsulated in its own housing, leading to mass, efficiency and accommodation challenges. Recently, the application of PCM within the scan cavity of a GEOS type satellite has been suggested, in order to tackle thermal issues due to direct sun intrusion (Choi, M., 2014). However, the application of PCM in such complex mechanical structures is extremely challenging. A new concept to tackle this issue is currently under development at the FH Aachen University of Applied Sciences. The concept "Infused Thermal Solutions (ITS)" is based on the idea to 3D print metallic structures in their regular functional shape, but double walled with internal lattice support structures, allowing the infusion of a PCM layer directly into the voids and eliminating the need for additional parts and interfaces. Together with OHB System, FH Aachen theoretically studied the application of this technology to the Meteosat Third Generation (MTG) Infra-Red Sounder (IRS) instrument. The study focuses on the scan cavity and entrance baffling assembly (EBA) of the IRS. It consists of thermal analyses, 3D-redesign and bread boarding of a scaled and PCM infused EBA version. In the thermal design of the alternative EBA, PCM was applied directly into the EBA, simulating the worst hot case sun intrusion of the mission. By applying 4kg of PCM (to a 60kg baffle) the EBA temperature excursions during sun intrusion were limited from 140K to 30K, leading to a significant thermo-opto-elastic performance gain. This paper introduces the ITS concept development status. Y1 - 2019 N1 - 49th International Conference on Environmental Systems, 7-11 July 2019, Boston, Massachusetts ; ICES-2019-72 SP - 1 EP - 14 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 -