Auflistung nach Schlagwort "aircraft design"

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  • Analyse der neuen LTH-Methode zur Massenschätzung von Flugzeugbaugruppen 
    Pape, Arlind (Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2018)
    In dieser Projektarbeit geht es um die Abschätzung von Massen der Hauptbaugruppen großer ziviler Verkehrsflugzeuge (MTOM > 40 t), sowie um die Abschätzung der Betriebsleermasse. Die Projektarbeit analysiert die 2013 im ...
  • Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion 
    Rodrigo, Clinton (Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2019)
    Purpose - This thesis presents a comparison of aircraft design concepts to identify the superior propulsion system model among turbo-hydraulic, turbo-electric and classic jet propulsion with respect to Direct Operating ...
  • Continuous Open Access Special Issue "Aircraft Design": Number 2/2020 
    Scholz, Dieter; Torenbeek, Egbert; CEAS Technical Committee Aircraft Design (TCAD); Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences (Basel : MDPI, 2020-12-31)
    Following the successful initial Special Issue on “Aircraft Design (SI-1/2017)”, this is already the second SI “Aircraft Design (SI-2/2020)”. Activities in the past showed that aircraft design may be a field too small to ...
  • Continuous Open Access Special Issue "Aircraft Design": Number 3/2021 
    Scholz, Dieter; Torenbeek, Egbert; CEAS Technical Committee Aircraft Design (TCAD); Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences (Basel : MDPI, 2021-12-31)
    Following the successful initial Special Issue on "Aircraft Design (SI-1/2017)" and the relaunch with "Aircraft Design (SI-2/2020)", this is already the third SI in sequence named "Aircraft Design (SI 3/2021)". Activities ...
  • Evaluating Aircraft with Electric and Hybrid Propulsion 
    Scholz, Dieter (Dorking, Surrey, UK : UKIP Media & Events, 2018)
    Purpose – This presentation takes a critical look at various electric air mobility concepts. With a clear focus on requirements and first principles applied to the technologies in question, it tries to bring inflated ...
  • Evaluation of the Hybrid-Electric Aircraft Project Airbus E-Fan X 
    Benegas Jayme, Diego (Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2019)
    Purpose - This master thesis evaluates the hybrid-electric aircraft project E-FAN X with respect to its economical and environmental performance in comparison to its reference aircraft, the BAe 146-100. The E-FAN X is ...
  • Flutter Characteristics of Typical Wing Sections of a Box Wing Aircraft Configuration 
    Fazelzadeh, S. Ahmad; Scholz, Dieter; Mazidi, Abbas; Friswell, Michael I. (Paris : Association Aéronautique et Astronautique de France (3AF), 2018)
    In this paper, the aeroelastic modeling and conceptual flutter analysis of a simple 2-D box wing is investigated. For each wing the torsion and bending elasticity is simulated by two torsional and longitudinal springs at ...
  • The Mass Growth Factor – Snowball Effects in Aircraft Design 
    Cheema, John Singh (Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2020)
    Purpose – This project work shows a literature survey, clearly defines the mass growth factor, shows a mass growth iteration, and derives an equation for a direct calculation of the factor (without iteration). Definite ...
  • Methoden zur Ermittlung des Betriebsleermassenanteils im Flugzeugentwurf 
    Lehnert, Jan (Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, 2018)
    Diese Projektarbeit beschäftigt sich mit dem Thema der Berechnung des Betriebsleermassenanteils im Flugzeugentwurf. Bekannte Berechnungsverfahren nach Torenbeek, Raymer, Marckwardt und Loftin werden auf Qualität und ...