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Aircraft Design and Sytems Group (AERO) @ Hamburg University of Applied Sciences - Prof. Dr. Scholz
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19 publications, page 1 of 2
(CSV)

  • Fallbeispiele zum Reverse Engineering im Passagierflugzeugentwurf

    Other literature type German OPEN
    Cheema, John Singh;
    (2019)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    Zweck - In dieser Bachelorarbeit werden die öffentlich nicht zugänglichen Technologieparameter von Passagierflugzeugen näherungsweise bestimmt. Das sind maximaler Auftriebsbeiwert bei Start und Landung, maximale Gleitzahl und spezifischer Kraftstoffverbrauch im Reiseflu...

  • Aerodynamic Analysis with Athena Vortex Lattice (AVL)

    Other literature type English OPEN
    Budziak, Kinga;
    (2015)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    This project evaluates the suitability and practicality of the program Athena Vortex Lattice (AVL) by Mark Drela. A short user guide was written to make it easier (especially for students) to get started with the program AVL. AVL was applied to calculate the induc...

  • Dynamic Cabin Air Contamination Calculation Theory

    Other literature type English OPEN
    Lakies, Marcel;
    (2019)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    In this report an equation is derived to calculate the dynamic effect of primary and secondary aircraft cabin air contamination. The equation is applied in order to understand implications and hazards. Primary contamination is from an outside source in form of normal lo...

  • Wartungskosten von Passagierflugzeugen bei verschiedener Triebwerksanzahl berechnet nach DOC-Methoden

    Other literature type German OPEN
    Niklas Brüge; Felix Kranich;
    (2018)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    Diese Projektarbeit versucht zu erklären, warum Flugzeuge mit drei oder vier Triebwerken kaum noch verkauft werden. Dabei wird insbesondere der Vermutung nachgegangen, dass Flugzeuge mit einer größeren Anzahl an Triebwerken höhere Wartungskosten haben könnten. ...

  • Conditions for Passenger Aircraft Minimum Fuel Consumption, Direct Operating Costs and Environmental Impact

    Other literature type English OPEN
    Caers, Brecht;
    (2019)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    Purpose - Find optimal flight and design parameters for three objectives: minimum fuel consumption, Direct Operating Costs (DOC), and environmental impact of a passenger jet aircraft. --- Approach - Combining multiple models (this includes aerodynamics, specific fuel...

  • Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion

    Other literature type English OPEN
    Rodrigo, Clinton;
    (2019)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    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 Costs (DOC), environmental impact and fuel burn. --...

  • Kraftstoffverbrauch durch Entnahme von Zapfluft und Wellenleistung von Strahltriebwerken

    Other literature type German OPEN
    Ahlefelder, Sebastian;
    (2006)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    Zapfluft und Wellenleistung wird den Triebwerken entnommen, um die Energie für beispielsweise die Kraftstoffpumpen, das Inflight Entertainment oder die Flügelvorderkantenenteisung zu erzeugen. Diese Energiegenerierung, hat einen Anstieg des Kraftstoffverbrauches zur Fol...

  • Methoden zur Ermittlung des Betriebsleermassenanteils im Flugzeugentwurf

    Other literature type German OPEN
    Lehnert, Jan;
    (2018)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    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 Aktualität untersucht und miteinander verglichen. ...

  • Aircraft Fuel Consumption - Estimation and Visualization

    Other literature type English OPEN
    Burzlaff, Marcus;
    (2017)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    In order to uncover the best kept secret in today's commercial aviation, this project deals with the calculation of fuel consumption of aircraft. With only the reference of the aircraft manufacturer's information, given within the airport planning documents, a method is...

  • Health Monitoring for Aircraft Systems using Decision Trees and Genetic Evolution

    Other literature type English OPEN
    Gerdes, Mike;
    (2019)
    Publisher: Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
    Reducing unscheduled maintenance is important for aircraft operators. There are significant costs if flights must be delayed or cancelled, for example, if spares are not available and have to be shipped across the world. This thesis describes three methods of aircraft h...
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