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Angefangen: Projekte, Bachelor- und Masterarbeiten

item 1. Prüfer: Prof. Dr.-Ing. Dieter Scholz, MSME

Name Thema Aufgabenstellung Typ der Arbeit In-/Ausland
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Anmeldedatum
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Abgabedatum
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Geheim VH
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E-Mail
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Tutor
Mohannad Chamas Conceptual Aircraft Design Using CEASIOMpy *.pdf

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.

Master Thesis Ausland SS21
27.05.21
Helios
27.11.21 nein J J DS
Ehsan Bazldost Calculating Aircraft Utilization How many hours can a passenger aircraft fly in one year? How many in one day? How many in one hour? How many flights each day? Block hours or flight hours? How much time needs to be reserved for maintenance, turn around, taxiing? All these questions can be answered from equations given in DOC methods. How do they compare? Can we find more on the Internet? Start with these documents: Script Aircraft Design: Design Evaluation / DOC, Chapter 14.3.10 and TU Berlin DOC Method. Project Inland WS21/22
02.11.21
Helios
02.05.22 nein J J DS
Sebastian Hirsch The 20 Most Important Parameters of the 50 Most Used Passenger Aircraft Define the 20 most important parameters of passenger aircraft. Find the 50 most used passenger aircraft. Collect the data (each number with a given source). Compare and curate the data. Display the data in Excel and HTML on the WWW. Write your project report. We have collected much data. It needs to be offered similar to this Aircraft Dataset. Master Project Inland WS21/22
16.10.21
Helios
22.05.22 nein J J DS
Dennis Lucht Numerical and Analytical Take-Off Field Length Calculations for Jet Aircraft *.pdf Bachelor Thesis Inland SS22
15.03.22
Helios
15.06.22 nein J J DS
Malte Lewerentz-Prohn Fuel Consumption of the 50 Most Used Passenger Aircraft Fuel consumption of passenger aircraft is certainly known, but for the public it is considered an industry secret. Not for us. Define fuel consumption of passenger aircraft. List and explain all public sources from which aircaft fuel consumption can be obtained directly or indirectly. I will guide you and show you the "secrets". Take the 50 most used passenger aircraft and list their fuel consumption in Excel and HTML on the WWW. Write your project report. Project Inland WS21/22
11.01.22
Helios
11.07.22 nein J J DS
Antonio Martínez Cano Fuselage Tank Location Trade-Off for Passenger Aircraft Powered with Liquid Hydrogen It seems to be advantageous, to store Liquid Hydrogen (LH2) in future passenger aircraft in the fuselage and to make the fuselage longer according to the required fuel volume. Two solutions are possible: 1.) a balanced aircraft configuration with one tank in the back of the fuselage and on tank aft of the cockpit, 2.) a less well balanced aircraft configuration (page 6) with two tanks (for reduncancy) both in the back of the fuselage . In solution 1.) the integration of the forward tank outside of the pressure cabin (for safety reasons) is difficult. Show solutions how this could be done. Estimate the increase in mass due to additional pressure bulk heads and similar additions related to the baseline. How does this translate to increased fuel consumption? In solution 2.) the shift in CG location will be larger. Start with a simple calculation to show the CG shift from full to empty tank expressed in percent MAC. Look at the chapter Empennage Sizing from the Aircraft Design lecture notes. Estimate by what percentage the horizontal tail will be larger on a less well balanced aircraft configuration (2) related to the baseline. How does this translate to mass and drag increase (and L/D reduction)? How does this translate to increased fuel consumption? Calculate with an Excel Table. Keep your calculations general, so that it is based on a set of input parameters. What is the better solution (1) or (2)? Master Thesis Ausland SS22
01.04.22
Helios
01.10.22 => 30.07.22 nein J J DS
Christian Rösing Application of the Trip Emission Ecolabel We launched an Ecolabel for Aircraft. Now we want to apply it in different ways. Here is one way to use the ecolabel: Assume you want to fly from Hamburg to Faro (Portugal) via Frankfurt. The first lag you fly in an A320neo and the second lag in an A321. You have the ecolabels of both aircraft. Now you can combine the information from the two ecolabels to get the total environmental burden of the two flights from: Fuel consumption, equivalent CO2, total local noise produced, and total local air pollution (NOx) produced. The results are given in the Trip Emission Ecolable (TEE). Certainly, also other connections are offered by other airlines or airline groups flying different aircraft. Such offers could be as a direct flight or with (more or less numbers of) stops at other airports. Your task is to calculate several interesting examples of TEEs. You will use existing software. Comment on your findings and derive general hints for passengers, when it comes to selecting a flight option form origin to destination, considering various offers found in flight booking engines. Project Inland WS21/22
30.01.22
Helios
30.07.22 nein J J DS
Salar Ali Digital Publishing in Engineering Research & Development *.pdf

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 already available. Your task is quite simple. You start writing from the first day. Based on the (mostly) Wikipedia articles given in the Table of Contents above you will find your way through the information presented on the Internet. As such, you will produce a report giving an introduction to all major aspects of "Digital Publishing in Engineering Research & Development".

Bachelor Thesis Inland SS22
09.05.22
Helios
09.08.22 nein J J DS
John Singh Cheema Ansätze für das Einführen effizienter Messsysteme zur Bestimmung der Dicke galvanischer Schichtsysteme auf Werkstücken in der Oberflächentechnik *.pdf Master Thesis Inland SS22
23.03.22
Helios
22.09.22 ja N-H J DS
Delgado Da Cruz, José Manuel and
Hatzetheodorou, Alexandros
NOx Emissions of the 50 Most Used Engines for Passenger Aircraft Nitrogen oxide is produced when nitrogen (N) and oxygen (O) are heated. NOx stands for any combination of N and O as explained here in detail. Inhalation of the pure NO and NO2 is rapidly fatal. NOx is also a potent greenhouse gas. NOx emissions of jet engines can be obtained from the WWW and can also be approximated with a method from Boeing (available as a spreadsheet). Collect and determine NOx emissions from jet engines. Compare and comment on your findings. Take the 50 most used engines for passenger aircraft. Disseminate your data in Excel-format and in HTML on the WWW. Write your project report. Project, Master Inland SS22
22.03.22
Helios
22.09.22 nein J J DS
Houssein Mahfouz Vergleich des Kraftstoffverbrauchs von Flugzeugen mit Strahltriebwerk und Propellertriebwerk Für Strahltriebwerke wird der Schub (N) angegeben. Für Propellertriebwerke wird die Leistung (W) angegeben. Die Leistung eines Strahltriebwerks könnte durch Multiplikation mit der Geschwindigkeit des Flugzeugs berechnet werden. Aber welche Geschwindigkeit ist damit genau gemeint? Bei beiden Triebwerkstypen ist der spezifische Kraftstoffverbrauch (Specific Fuel Consumption, SFC) unterschiedlich definiert: kg/(Ns) versus kg/(Ws). Wie lässt sich der Kraftstoffverbrauch beider Triebwerkstypen vergleichen? Kann man den (dimensionslosen) Wirkungsgrad der Triebwerke nutzen? Wie sieht der Vergleich aus zwischen einem Kolbenmotor mit Propeller und einem Propellerturbinenluftstrahltriebwerk (PTL)? Ist es fair, einen Verbrennungsmotor mit einem Elektromotor zu vergleichen? Nein, aber warum nicht? Manchmal werden Energiewandler an Bord (Brennstoffzellen oder Leistungsentnahmen vom Triebwerk) mit den eigentlichen Triebwerken verwechselt! ... Projekt, Master Inland SS22
04.04.22
Helios
04.10.22 nein J J DS
Tobias Albrecht Design of a Modern Passenger Aircraft with Diesel-Engine and Propeller Background is this Video and the review of data for the preparation of the short documentary. See also here. Task is to take the Top Level Aircraft Requirements (TLARs) of the A320 or A320neo and to design an aircraft with this engine type. You may want to look at our (re)designs of the ATR 72 and "Smart Turboprop". Project, Master Inland SS22
11.04.22
Helios
11.10.22 nein J J DS
Martin Gollnow Passenger Aircraft towards Zero Emission with Hydrogen and Fuel Cells Requirements: 120 .. 200 pax, 2000 NM, cruise Mach number 0.78 (i.e. the reference are the A320 TLAR). Technology: Fuel cell. Fuel: LH2. Is the design feasible? Design for different objectives (minimum of ...): DOC, fuel, primary energy, climate impact, environmental impact (climate & resources). The major environmental effect depends on cruise altitude and Aviation Induced Cloudiness (AIC). Can the water be collected in a tank and transported down? Can the water be transformed into ice cubes that are discarded over board? Project Inland SS22
16.05.22
Helios
16.11.22 nein J J DS

 

Die folgenden Arbeiten wurden bereits abgegeben
eine (vollständige) Aufarbeitung zur Veröffentlichung im Netz steht aber noch aus!
Name Thema Aufgabenstellung Typ der Arbeit In-/Ausland
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Anmeldedatum
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Abgabedatum
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Geheim Bew.
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Tutor
Marlis Krull Preliminary Sizing of Propeller Aircraft (Part 25) PreSTo-Classic is available not only for jet aircraft (jets) but also for propeller driven aircraft (props) certified for CS-25 respectively FAR Part 25. The initial task is to implement a more sophisticated method for propeller efficiency estimation and to automate the iteration(s) related to propeller efficiency estimation in Excel. It follows an Excel table "PreSTo-Classic-Prop", which should be tested with the redesign of a large passenger propeller aircraft. If time allows, "PreSTo-Classic-Prop" could be adapted also for optimization. How this works, is shown by the project SAS - Simple Aircraft Sizing, where an optimization Excel spreadsheet is already available for large jets, but one for large props (CS-25) is still missing. Project Inland WS21/22
29.10.21
Helios
29.04.22 nein N DS
Shirin Salehi Comparing Modes of Transportation with an Improved Kármán–Gabrielli Diagram

The start of the considerations is:

GABRIELLI, G., von KARMAN, Th., 1950: What price speed? Specific power required for propulsion of vehicles. Mechanical Engineering, vol. 72 (1950), no.10, pp. 775-781. Available from: https://perma.cc/5FZH-YGTR

Three parameters are collected for each mode of tranportation: total weight (W), max. power (P) and max. speed (V). P/(W*V) is called "specific power". The idea was revisited in 2005 (https://perma.cc/43XQ-BJRW). Now P/(W*V) is called "specific resistance". The concept is discussed further e.g. on Wikipedia. Now the inverse is used: (W*V)/P = W/D = L/D, with lift (L) and drag (D) we get the well know glide ratio (L over D). In this new way, the "Kármán Gabrielli Diagram" (KG Diagram) may be plotted like this. Moreover, P/(W*V) with V=s/t can also be understood as a proxy of (P*t)/(s*W) can be understood as fuel consumption per weight. The plot shows a technology limit. Specific resistance is proportional to speed. This means, we have to pay for speed. This is the answer to the original question: "What price speed". But for the same speed some modes of transportation are better than others. Which modes of transportation are better in general? Which in aviation? Task is to look at the critique of the KG Diagram:

  • Only the percentage of power should be considered which is used in cruise. 
  • Cruise speed should be used not max. speed.
  • Payload should be used instead of total weight.
  • Instead of shaft power and speed, fuel consumption should be used, or even better primary energy consumption.

Ways to overcome the KG simplifications should be proposed as well as applied and the results should be discussed.

Project Inland WS21/22
16.10.21
Helios
16.04.22 nein J DS
Philipp Gmelin Signal Transmission between Electrical Components in Microlight Aircraft *.pdf Bachelor Thesis Inland WS21/22
29.11.21
Helios
01.03.22 nein J DS
Diego Fonseca Direct Operating Costs, Fuel Consumption, and Cabin Layout of the Airbus A321LR *.pdf Bachelor Thesis Inland WS21/22
09.09.21
Helios
09.12.21 nein J DS
Niklas Brüge, Felix Kranich Estimation of an Aircraft's Effective Perceived Noise Level from Its Basic Parameters A realistic simulation of aircraft noise during take-off and landing is impossible with simple methods. Nevertheless, simple methods are needed in preliminary aircraft design, if aircraft parameters should be optimized early on - also to the benefit of designing a low(er) noise aircraft. A suitable approach is, to estimate Effective Perceived Noise Levels based on established correlations between basic aircraft parameters and the aircraft's noise level. Proposals can be found in the literature (here and here). Task is to make a literature review to get an overview of such methods, select a simple method and build a spreadsheet (Excel) with which the selected method can be used with ease. Master Project Inland WS20/21
03.10.20
In Helios:
SS20
15.05.20 V nein J DS
Mohamed Oussama Hammami Turbofan Specific Fuel Consumption, Size and Mass from Correlated Engine Parameters *.pdf Master Thesis Inland SS21
15.03.21
In Helios:
SS21
15.09.21 nein J DS
Mehmet Öcalan Kontamination des Trinkwassers in Flugzeugen durch Mikroorganismen und Metalle *.pdf Bachelor Thesis Inland WS20/21
27.01.21
In Helios:
SS21
29.09.21 VV nein J DS
Philipp Gmelin Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing *.pdf Project Inland WS20/21
27.10.20
Helios
27.04.20 nein J DS
David Delgado del Río Revealing the Technical Secrets of the 40 Most Used Passenger Aircraft with Reverse Engineering Am Excel-File is available with a program that facilitates to reverse engineer aircraft (at the level of aircraft design). The program was the outcome of a Master Thesis. The program is well documented. A big secret of an engine manufacturer is the Specific Fuel Consumption (SFC) of the jet engine. A big secret of an aircraft manufacturer is the aerodynamic efficiency expressed by the maximum ratio of lift over drag (L/D)_max. Another secret of the aircraft manufacturer is the maximum lift coefficient of the aircraft. We want to offer the aircraft design community a very good assumption of mainly these three parameters (and some "byproducts"). The 40 most used passenger aircraft types together serve over 90% of all the passenger flights in the world. Master Thesis Ausland SS20
31.05.20
Helios
31.08.20 nein J DS
Dennis Tietke Comparison of Potential Oil Leakage of Jet Engines - Evaluation of Design Parameters Cabin Air Contamination (details here) is caused by leakage through the seals of jet engines. Jet engines have heavy shafts supported by bearings. They are lubricated and sealed. These seals leak small amounts of oil by design. The leackage related concentration of hydrocarbons in the cabin depends not only on the amount of oil leaving the seals, but also on a set of engine and aircraft parameters, because not all of the oil can reach the cabin. The parameters are combined in one simple equation. We look at a number of dominant jet aircraft and their engines in order to calculate the cabin air contamination potential. A comparison may reveal aircraft-engine-combinations more prone to cabin air contamination than others based already on external design parameters. Project Inland WS19-20
25.09.19
Helios
25.03.19 nein J DS
Tim Maximilian Jansen Analysis of Data from FlightRadar24.com for Aircraft Design and Performance Based on FlightRadar24 Data Services (example: A350 from Vienna to Taipei), flight data should be analysed to learn about (e.g.) cruise speed (TAS) and flight altitude, step climbs, initial cruise altitude, taxi time, holding time with altitude and speed, ... Comparison of aircraft, ... Project Inland WS19-20
25.09.19
Helios
25.03.19 nein J DS
Taner Ayan Analyse der Liegezeiten von Passagierflugzeugen nach Fume Events mittels Flugverfolgung Fume Events präziser Cabin Air Contamination Events (CACE) sind Ereignisse bei denen die Kabinenluft von Passagierflugzeugen kontaminiert wird. In schweren Fällen ist die Kabine durch Rauch (fumes) erfüllt. Die Kontamination kann durch giftige Stoffe aus dem Triebwerksöl verursacht sein. Dadurch können Besatzung und Passagiere kurzfristige und chronische Gesundheitsschäden erleiden. Die Kontamination der Kabinenluft kann zur Flugunfähigkeit der Piloten führen und stellt dadurch eine Gefahr für die Flugsicherheit dar. Flugzeughersteller haben Anweisungen herausgegeben, wie ein Flugzeug nach einem Fume Event zu reinigen sei. Ziel dieser Untersuchung ist, eine Liste mit aktuellen Fume Events zu erstellen, die entsprechenden Flüge mit Onlinediensten zur Flugverfolung zu identifizieren, die Dauer einer eventuellen sich anschließenden Liegezeit zu erfassen und diese mit den Reinigungsanweisungen zu vergleichen. Projekt Inland WS19-20
21.10.19
Helios
21.04.19 nein J DS
Laura Salcedo Campoamor Calculating the Power of Wind Turbines with the Blade Element Momentum Theory A) Literature review of available free tools to calculated the aerodynamic power output of wind turbines. B) Programming of an Excel-based tool to estimate the aerodynamic power output of wind turbines with the Blade Element Momentum Theory (BEM) - allowing also for limited wind turbine optimization.

Please see also my (old, but still valid) student work on wind energy at Hannover University.

Master Thesis Ausland SS17
20.03.17
Helios
E-Mail, FSB
10.09.17 nein J DS
Nicolai Lützen,
Amine Bahrani
Aerodynamic Investigation of C-Wings with Tornado Tornado is a vortex lattice method implemented in Matlab. It is used here to calculate the lift distribution especially on the upper horizontal part of the C-wing to understand the concept. Tornado is also used to calculate the induced drag of C-wings of different shapes (in comparison to the reference wing without a wing tip device). Aim is to confirm or correct the handbook method as given in the paper Estimating the Oswald Factor from Basic Aircraft Geometrical Parameters. Project Inland WS16/17
09.10.16/26.10.16
Helios
V 12.07.17 nein J DS
David Schubert Wirtschaftlichkeit eines Airbus A380 mit neuen Triebwerken Airbus considers launching an A380neo. With a classical design study, we look at how parameters will match up. Project Inland WS16/17
22.09.16
Helios
V 22.05.17 nein J DS
Rachna Harsh Creating Interactive Elements for an "Aircraft Design" "Open Educational Resource" (OER) This is the Aircraft Design OER. It includes this interactive element Task was to design more interactive elements for the Aircraft Design OER with H5P like drag-the-words, fill-in-the-blanks, image-hotspot-question, mark-the-words, multichoice, personality-quiz or questionnaire (to let user design aircraft), question-set(!!!), single-choice-set, summary, true-false or maybe even an interactive-video. Idea: Activate students with design activities and interactive questions so that learning is even more fun.

The results of this project can now be found here.

Bachelor Thesis Ausland SS17
20.03.17
Helios
E-Mail, FSB
03.09.17 nein J DS
Peter Löwen,
Marco Krause
Publishing a Dataset with Aircraft Parameters in a Data Repository Research data should be stored in a data repository. See also this picture. We will look at various repositories like the Harvard Dataverse Network. We will then accumulate aircraft data from many sources on the Internet. On such source is Jenkinson's Dataset. Eventually we will make our dataset available to the world in a professional way according to current standards. Team Project Inland Krause:
WS15/16
??.??.??
Helios

Löwen:
WS16/17
27.09.16
Helios

27.03.17 nein J DS
Lennart Hildebrandt,
Nemo Juchmann
Analyse der Flugdynamik in den Flugsimulatoren FSX und X-Plane Vergleich von realen flugdynamischen Eigenschaften ausgewählter Flugzeugmuster (selbst erflogen oder aus Tabellen) mit den aus herkömmlichen Flugsimulatoren (FSX, X-Plane 10) erflogenen Eigenschaften. Dies soll erste Hinweise geben auf die Güte dieser Flugsimulatoren. Projekt im Team Inland SS16
05./06.04.16
Helios
V: 24.11.16 nein J DS
Alexander Broer Verbesserung des aerodynamischen Modells zur Berechnung von Böenlasten auf Passagierflugzeuge Bestandteil der BA Bachelor Arbeit Inland SS16
22.06.16
E-Mail, FSB
10.09.16 ja J DS
Wim Breugelmans Predicting Buffet Onset in Conceptual Aircraft Design A method to quickly compute the buffet envelope of a new aircraft geometry is given in the literature. The method is semi-empirical. It uses a combination of simple sweep theory and a buffet onset boundary of a given seed aircraft (alternatively, any other aircraft could be used as seed aircraft if the buffet onset boundary is available). Aim is to estimate the buffet onset boundary of a target geometry already at the conceptual design stage. The method should be described, programed in Excel, and applied. Wherever possible, the results should be compared with real aircraft characteristics. Master Thesis Ausland SS16
17.03.16
Helios
SS16 nein J DS
Kevin Catrysse Cruise Speed Reduction (CSR) - Aerodynamic, Flight Mechanic, and Economic Effects I have explained the basics here. Various of our studies show also Direct Operating Costs (DOC) reduction due to CSR. See how an optimized A320 could benefit in this dissertation. See also our publications about the slow flying Smart Turboprop: here and here. Authors looked also with more detail at the effects caused by CSR applied in the air transportation network e.g. here. Task is to make a full Internet review of CSR and to put all the arguments for and against CSR in a concise and logical sequence. Master Thesis Ausland SS16
17.03.16
Helios
SS16 nein J DS
Clara Simón García Aircraft Simulation and Analysis with HOPSAN-NG The simulation program HOPSAN in its new version (HOPSAN-NG) allows a wide range of simulations from the aircraft hydraulic system, via aircraft dynamics up to the simulation of a whole aircraft mission based on pre-defined way points. According to the developers (who will support us) this should allow an evaluation of the aircraft including its fuel consumption and many more other details. The task is to verify this claim and to judge HOPSAN for its suitability as an analysis tool in aircraft design. Bachelor Thesis Ausland SS16
17.03.16
Helios
SS16 nein J DS
Mia Eder G. Corning's Airplane Design Methodology As early as 1953 Gerald Corning, professor at the University of Maryland, devised a method for his students for the layout of subsonic passenger aircraft. Starting from requirements and ending at Direct Operating Costs. The method is given in his book Supersonic and subsonic airplane design (published by the author, in 1953 and 1960) in Chapter II. Task is to put the method in a clear and easy understandable sequence, to update some of the parameters to current technology levels, and to make the method available in form of a spreadsheet. Project Inland --- --- nein J DS
Karim Drews Bulk or Containerized Loading of Narrow-Body and Wide-Body Aircraft - What to Prefer? Airlines have the choice if they want to use container to load baggage or if suitcases are stored one by one in the cargo compartment. Cargo is mostly loaded in container. Smaller aircraft do not offer containerized loading. MD90 and Dash8 aircraft may operate with bulk baggage container. Wide-body aircraft use mostly the LD-3 type container. The narrow-body Airbus A320 can accommodate LD-3 container with reduced height. Hence some interline compatibility is offered between narrow- and wide-body aircraft. Container allow a quicker turn around of the aircraft leading to a higher utilization and potentially reducing Direct Operation Costs (DOC). Nevertheless, container add weight that reduces payload. Container require additional investment leading to depreciation and additional costs. In the end the preferred choice is a trade-off between depreciation, payload, and turn around time respectively turn around costs. See also: SKYbrary. This task may lead to an exchange of ideas with Etihad Airways. Project Inland --- --- nein J DS
Tim Haß Eco Lables for Aircraft *.pdf Bachelor Thesis Inland SS15
05.06.15
Helios
05.08.15 nein J DS
Johann Metzger Analyse des Sinkfluges von Germanwings 4U9525 I started with calculations of the Airbus A320's flight based only on a few points in time during the descent. A more detailed calculation will include more time steps, investigate more parameters (wind speed), and put everything in a comprehensive table. This table will be based on elementary data from FlightRadar24 or other available data at the time of writing. It will calculate depending parameters and compare these with published data. The result will be a set of parameters consistently describing the descent of 4U9525 also including parameters of the aircraft's aerodynamics and flight modes according to the autopilot logic and Fly-by-Wire flight control laws. Projekt Inland --- --- nein J DS
Aqib Khan Fuel Consumption during Extreme Long and Short Flights The average fuel consumption expressed in kg/100 km is relatively high for very long flights, but also for very short flights. Plotting fuel consumption versus flight distance we expect to get a typical "bath tub curve". This curve should be analyzed and discussed. Bachelor Thesis Ausland SS15
26.06.15?
E-Mail, Korn
07/2015 nein J DS
Deepam Mishra Using OpenVSP for Aircraft Design OpenVSP is a tool from NASA. Task is to check OpenVSP Version 3.0 for new features and compatibility with OpenVSP Version 2.0. Advanced features should be used in trials as far as possible. Bachelor Thesis Ausland SS15
26.06.15?
E-Mail, Korn
07/2015 nein J DS
Raghu Nandan Singh Optimization of Very Light Aircraft (VLA) Summarize requirements for these aircraft form certification standards as they influence prelimianry aircraft design. Select an example aircraft from this class and optimize its design by modifying already existing software from the project SAS. Master Thesis Ausland SS15
24.06.15
E-Mail, Korn
07/2015 nein J DS
Ramachandran Karunanidhi Aviation Fuel for the Future - Methane Hydrate Possibilities of using methane hydrate as the source of energy for air transportation. Project Ausland WS14/15
11/2014
Helios
05/2015 nein J DS
Tom Alisch Alternativen zur Hilfsgasturbine (APU) Die Option ohne APU zu fliegen generiert Vorteile beim Flugzeuggewicht und den Wartungskosten des Systems. Es bedeutet aber gleichfalls eine gesteigerte Abhängigkeit der Bodenversorgung mit Sekundärenergie. Projekt Inland WS14/15
21.10.14
Helios
21.04.15 nein J DS
Hairul Nahar Bin Nasir Empennage Sizing with the Tail Volume Coefficient - Basic Statistics Projektbericht wurde nicht abgegeben. Projekt Ausland WS14/15
18.11.14
E-Mail, Korn
18.05.15 nein J DS
Sayin, Aytac Empennage Sizing with the Tail Volume Coefficient - Basic Statistics Projektbericht wurde nicht abgegeben. Projekt Ausland WS14/15
19.11.2014
E-Mail, Korn
19.05.15 nein J DS
Muhamad Shafeez Shaharan Interactive Cabin and Fuselage Layout with PreSTo *.pdf Bachelor Thesis Inland WS14/15
23.10.2014
Helios
23.01.15 nein J DS
Joshua Brechlin Induced Drag of Box Wing Aircraft - Variation of Aspect Ratio, Sweep and Taper Ratio Projektbericht wurde nicht abgegeben. Projekt Inland WS13/14
03.12.13
11.07.14 V nein J DS
Veselin Pavlov Aircraft 3D-Modeling with OpenVSP-Connect NASA offers the tool Open Vehicle Sketch Pad (OpenVSP). OpenVSP-Connect from AERO at Hamburg University of Applied Sciences Hamburg is an interface tool between any Excel based aircraft design tool and OpenVSP. OpenVSP-Connect is an Excel based tool which uses Visual Basic Macros. It needs 46 aircraft (geometry) parameters in order to provide a 3D visualization of a designed aircraft. The software never asks for a parameter without suggesting one first or giving a value by default. First objective is to improve OpenVSP-Connect such that it can be used as a self-contained tool which estimates all necessary 46 parameters from an hand full of requirements to visualize an aircraft. Second objective is to show how to incorporate OpenVSP-Connect in any already existing tool chain. In this way OpenVSP-Connect should also provide the missing link between any other aircraft design tool made by the AERO, i.e. Aircraft Preliminary Sizing Tool (PreSTo) and OpenVSP. Project Ausland SS14
05.05.14
Helios
11.07.14 nein J DS
Maxime van Loo Aircraft Wing Design with the Open Software PreSTo *.pdf Master Thesis Ausland SS14
19.06.14
E-Mail, Korn
11.07.14 nein J DS
Johan Peterson An Optional APU for Passenger Aircraft *.pdf Project Ausland SS14
19.06.14
E-Mail, Korn
11.07.14 nein J DS
Sowmya Thyagarajan Mass Estimation with the LTH/DLR-Method The German Aerospace Center (DLR) has published a simple, parametric method in the German Aeronautical Handbook (Luftfahrt Technisches Handbuch - LTH) to estimate the mass of major aircraft components. The method is called: "Large Civil Jet Transport (MTOM > 40t), Statistical Mass Estimation, MA401". The project compares the method with the one given in "Torenbeek" with respect to approach and accuracy.

Paper written from this project work at HAW Hamburg: http://www.ijemr.net/DOC/AircraftMassEstimationMethods(170-178).pdf. Archived at: https://perma.cc/PEN6-Z545.

Project Ausland SS14
19.06.14
E-Mail, Korn
11.07.14 nein J DS
Zubin Mistry Aircraft Design with VAMPzero Comment on the theory of the method and work an example. Download from http://vampzero.sourceforge.net Project Ausland SS14
19.06.14
E-Mail, Korn
07.07.14 nein J DS
Elena García Llorente Conceptual Design Optimization of Passenger Box Wing Aircraft in Biplane Layout *.pdf Master Thesis Ausland WS13/14
01.10.13
E-Mail, Korn
17.02.14 nein J AJ/DS
Mia Eder Parabelflüge mit Kleinflugzeugen *.pdf Projekt Inland SS13
27.03.13
23.12.13 VV nein J DS
Karim Drews Grundlagen zur Triebwerksintegration mit statistischen Betrachtungen *.pdf Projekt Inland SS13
21.03.13
05.01.14 VV nein J DS
Roberto Segovia García Turboprop Aircraft Design Optimization - Tool Development *.pdf Master Thesis Ausland SS13
30.08.13 nein J AJ/DS
Elien Verheire Systematic Evaluation of Alternative Box Wing Aircraft Configurations *.pdf
For visualisation:
Open VSP
Bachelor Thesis Ausland SS13 12.07.13 nein J PB/DS
Martin Fekete Induced Drag of Box Wing Aircraft - Variation of Decalage and Vertical Separation *.pdf Project Ausland SS13 12.07.13 nein J RC/DS
Haider Riaz Induced Drag of Box Wing Aircraft - Variation of Dihedral --- Project Ausland SS13 12.07.13 nein J RC/DS
Benjamin Hochart Integraton of the Wing Module into the PreSTo Suite --- Project Ausland SS13 12.07.13 nein J RC/DS
Elena Behrendt Bodenabfertigung eines BWB --- Projekt --- --- 29.04.13 nein J DS
Michel Pinck Dimensionierung der Fenster und Frachttore von Passagierflugzeugen *.pdf Projekt --- --- 23.03.13 nein J DS
Luis Salord Losantos Estimating E_max for Turboprop Aircraft *.pdf Memo --- --- 13.07.12 nein J AJ
Hoa Ly Life-Cycle Assessment of Commercial Aircraft – A Review of Methods and Tools *.pdf Project --- --- 13.07.12
(22.09.12)
nein J AJ
Jeroen Verstraete Creating a Life-Cycle Assessment of an Aircraft *.pdf Project --- --- 13.07.12
(26.09.12)
nein J AJ
Nishant Bhanot Modeling of a Turboprop Driven Aircraft using PlaneMaker for Flight Simulation with X-Plane *.pdf Project --- --- 20.07.12 nein J AJ
Sameer Ahmed Family Concepts of Box Wing Aircraft *.pdf Project --- --- 10.08.12 nein J DaS
Ricardo Caja Calleja Flight Dynamics Analysis of a Medium Range Box Wing Aircraft *.pdf Master Thesis --- --- 30.06.12 nein J DaS
Ricardo Caja Calleja Flight Dynamics Model of a Box Wing Aircraft using JSBSim *.pdf Project --- --- 24.10.12 nein J DaS
Jeremy Bouten Using X-Plane for Analyzing Aircraft Performance *.pdf Project --- --- 13.07.12
(22.09.12)
nein J DaS
Tayfun Süle Programmierung einer Schnittstelle zwischen PreSTo and CATIA *.pdf Projekt --- --- 15.07.11 V nein J DS

 

* In-/Ausland:
Inland: Studierender ist regulär an der HAW Hamburg eingeschrieben.
Ausland: Studierender ist Gaststudent aus dem Ausland. Hier gibt es andere Abläufe im Fakultäts Service Büro (FSB).

** Anmeldedatum:
Projekte sind teilweise ohne Anmeldedatum in Helios. Anmeldedatum ist daher das Datum der E-Mail-Bestätigung von Frau Korn.

*** Abgabedatum:
Abgabe für Projekte ist 6 Monate nach Ausgabe des Themas von mir (nicht etwa 6 Monate nach Anmeldung in Helios). V: Termin unter Berücksichtigung der gewährten Verlängerung.
Abgabe für Bachelorarbeiten ist 3 Monate nach Anmeldung in Helios (regulär) oder 2 Monate nach Anmeldung in Helios (Bachelorarbeit getrennt von Praktikum).
Abgabe für Masterarbeiten ist 6 Monate nach Anmeldung in Helios.

**** VH:
Vereinbarung unterschrieben? Anmeldung in HELIOS?     J: ja     N: nein     N-H: nein, aber bereits in HELIOS     N-V: nein, aber Vereinbarung bereits unterschrieben

***** E-Mail:
E-Mail mit den Hinweisen zum wissenschaftlichen Schreiben verschickt und perma.cc eingerichtet (V); erhalten und bestätigt mit ja (J).

****** Bew.:
Bewertung:     J: ja     N: nein     J/DL: ja und bereits eingestellt in der Digital Library - Projects & Theses - Prof. Dr. Scholz

Tutor:
AJ:    Andreas Johanning
DaS:  Daniel Schiktanz
DS:   Dieter Scholz
PB:   Priyanka Barua
RC:   Ricardo Caja
TS:   Tahir Sousa

Die Stundenabrechnung für im SS angemeldete Arbeiten erfolgt im darauf folgenden WS.
Die Stundenabrechnung für im WS angemeldete Arbeiten erfolgt im darauf folgenden SS.


STAND:  16. 05. 2022
AUTOR:  Prof. Dr. Scholz
IMPRESSUM (PDF)

E-Mail-Adresse
home  Prof. Dr. Scholz
home  Aircraft Design and Systems Group (AERO)
home  Studiengang Flugzeugbau
home  Department Fahrzeugtechnik und Flugzeugbau
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