Angeboten: Projekte, Bachelor- und Masterarbeiten

Arbeiten am Department Fahrzeugtechnik und Flugzeugbau, Prüfer: Prof. Scholz

Bachelorarbeit bei mir - wie geht das rechtlich?

§ 4 Vorpraxis und praxisbezogene Studienanteile (Zu § 6 APSO-INGI)
(2) In den Studiengängen Fahrzeugbau und Flugzeugbau ist ein von der Hochschule gelenktes industrielles Projekt bestehend aus Praxisphase und Bachelorarbeit von insgesamt 22 Wochen Dauer [!!!=5,5 Monate!!!] ... im siebten Semester durchzuführen. Das industrielle Projekt ist vorzugsweise im industriellen Berufsfeld des Fahrzeugbau- oder Flugzeugbauingenieurs durchzuführen.

§ 7 Praxisphase und Bachelorarbeit (Zu § 15 APSO-INGI)
(4) Die Bearbeitungsdauer der Bachelorarbeit beträgt drei Monate.
(6) Entscheiden sich die Studierenden, die Praxisphase und die Bachelorarbeit in mehreren Einrichtungen oder Betrieben durchzuführen [die BACHELORARBEIT AN DER HAW HAMBURG bei mir], kann dieses in Praxisphase (15 CP) und Bachelorarbeit mit Kolloquium (15 CP) [also BACHELORARBEIT bei mir] getrennt werden. Die Trennung ist bei dem jeweiligen Praktikumsbeauftragten für das industrielle Projekt zu beantragen [DAS GEHT SCHRIFTLICH FORMLOS OHNE SCHWIERIGKEITEN]. In diesem Fall beträgt die getrennt von der Bachelorarbeit ablaufende Praxisphase [nur noch] zwei Monate [!!!] ..., die Bearbeitungsdauer der Bachelorarbeit bleibt unverändert. [!!! Sie sparen dabei sogar noch 2 Wochen !!!]

Gibt es auch etwas einfachere/schnellere Projekte?

Liste der Angebote / Tasks Offered

Thema / Topic	Typ der Arbeit / Type of Work	Aufgabenstellung / Task	Status
Design of the New Ultra-Efficient NASA-Funded B737	Thesis or Project	Read about the funding for a new Boeing 737 design and come up with your proposal for this new clean sheet design.	available
Design of a Hydrogen Near Zero Emission Passenger Aircraft	Master Thesis	Requirements: 120 .. 200 pax, 2000 NM, cruise Mach number 0.78 (i.e. the reference are the A320 TLAR) Technology options (and combinations): Hydrogen turbofan or turboprop, hybrid with fuel cell and embedded electric motor (for boost or cruise). Fuel options: LH2 (new design), synthetic fuel (drop-in fuel). Design for different objectives (minimum of ...): DOC, fuel, primary energy, climate impact, environmental impact (climate & resources). Note: Zero emission (zero climate impact) is impossible. Burning hydrogen produces water and NOx. It is primarily NOT about "decarbonization". The major environmental effect depends on cruise altitude and Aviation Induced Cloudiness (AIC). Aviation has a water problem more than a CO2 problem. All considerations have to be based on a Life Cycle Analysis (LCA) and its "Single Score".	available
Optimization in Aircraft Design with Excel's "Solver"	Thesis	In the research project SAS (Simple Aircraft Sizing) we have developed optimization tools to support the first step in Aircraft Design called Preliminary Sizing. All of these little tools use an Evolutionary Algorithm (EA) of type Differential Evolution (DE). The Excel Solver has been used only as part of the global Differential Evolution. This is described in the Dissertation (PDF, 10 MB) in Chapter 6.2 and 7.3.3. The dissertation was part of OPerA. In order so simplify the tools from SAS, we want to find out, if we can also produce a tool for Preliminary Aircraft Design that makes use only of Excel's Solver.	available
Proposing a Classification for Aeronautics, Astronautics, and Aerospace Sciences	Project	Classifications - the heart of science. Examples of classifications are DDC (German), ICD-11, and other standard classifications. For the task here, please have a look at this: A first idea to get started (written by myself). What other classifications exist in our field of Aeronautics, Astronautics, and Aerospace Sciences? What is the best and most suitable one? What are applications for such a classification (apart from the publishing industry)?	available
Digital Publishing in Engineering Research & Development	Project or Thesis	As an individual in a company or as part of the international science community the need arises to communicate/disseminate your work results among your peers. Today the communication and/or dissemination will primarily be digital, but in most cases still traditionally based on writing. Other means of digital communication (voice, graphical, video, data centered) are possible, but not the main focus of this task. A company would have (hopefully) defined its product centered communication strategies and standards. Information will primarily be pushed through the organization as need to know requires. Corporate research results are archived and kept secret, protected by patents, or shared with the international science community. In the international science community, the information is rather pulled by researchers in literature reviews. For this reason, researchers make their results publically available in established databases and/or consider alternative means of dissemination through the Internet. The project gives an overview of the various modern digital publishing concepts and provides students with a hands-on experience ranging from scientific writing to publishing strategies for their own career development, be it in industry or academia. A proposed Table of Contents is also available. Your task is to write a report about all major aspects of "Digital Publishing in Engineering Research & Development".	available
Evaluation of the Aircraft Design and Analysis Software (ADAS)	Project	ADAS is an Excel-based tool written at the University of Naples. Try out the program and write about your experience with it. Here in the 2011 EWADE Presentation you can get a first idea of what it is all about.	available
Reserved:
Effiziente kontaktlose Messverfahren für galvanische Schichtsysteme auf Werkstücken der Luftfahrttechnik	Master Thesis	TBD	reserved
Direct Operating Costs and Fuel Consumption of the Airbus A321LR	Bachelor Thesis	The Airbus 321LR exchanges number of seat (payload) for fuel (range). As such the aircraft burns more fuel for less passengers on more range. Collect data from here and from other places on the Internet. How does this influence the fuel consumption expressed in kg per seat and per km flown? How do the A321LR Direct Operating Costs (DOC) compare to an A321neo as well as an A330neo and/or A350? Comment on official company and press statements like this on: "The LR’s range of up to 4,000 nautical miles is made possible by three additional centre fuel tanks and the aircraft delivers 30% fuel savings ... compared to previous generations of aircraft" (https://perma.cc/F3R6-YH82). Compare the aircraft's fuel consumption with the "bath tub curve" as explained by Burzlaff. Use the AEA Method and/or the TU Berlin Method to calculate DOCs. Compare the A321LR with competing types based on our Ecolabel for Aircraft.	reserved
Software Testing: Rapid Air System Concept Exploration (RASCE)	Bachelor Thesis	RASCE is an Excel-based aircraft design tool which is offered as "Complimentary Program" to OpenVSP (www.openvsp.org). RASCE comes in four versions. We are most interested in the turbofan design tool. Check out the tool and redesign a selected aircraft. Compare with the aircraft design tools used in my lecture (http://fe.ProfScholz.de) and research group (software will be provided). You could even compare with ADAS (see task below). What can we learn or add from RASCE? Links: http://www.openvsp.org/wiki/doku.php?id=rasce http://www.openvsp.org/wiki/lib/exe/fetch.php?media=rasce:f2009.rasce_overview.pdf RASCE for Turbofan Aircraft: http://www.openvsp.org/wiki/lib/exe/fetch.php?media=rasce:rasce.tbfan.2009.xls	reserved
Conceptual Aircraft Design Using CEASIOMpy	Master Thesis	CEASIOMpy is a conceptual aircraft design environment. CEASIOMpy can be used to set up complex design and optimization workflows, both for conventional and unconventional configurations. Tools for various disciplines in aircraft design are provided, amongst others: aerodynamics, weight and balance, flight mechanics, structures, aeroelasticity. Please find details here: https://ceasiompy.readthedocs.io https://github.com/cfsengineering/CEASIOMpy Compare also with the Master Thesis written by Maria Pester in 2010 archived in http://library.ProfScholz.de.	reserved
Analytical Balanced Field Length Estimation	Bachelor Thesis	Calculation of the balanced field length (BFL) traditionally involves a numerical calculation, where the various forces are evaluated as a function of speed, using a step-wise integration and an estimate for V1. The process is iterated with different values for the engine failure speed until the accelerate-stop and accelerate-go distances are equal. Are there simple analytical methods to estimate BFL? (See: Thesis Ehrig, SAE-Paper [new link!] or Raymer)	reserved

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  Prof. Dr. Scholz
  Aircraft Design and Systems Group (AERO)
  Studiengang Flugzeugbau
  Department Fahrzeugtechnik und Flugzeugbau
  Fakultät Technik und Informatik
  HAW Hamburg