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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
Mohan Pannirselvam TBD   Projekt im Master Inland WS19-20
11.11.19
Helios
11.05.20 nein N-H V DS
Lena Peter Social Evaluation of Aircraft The Life Cycle Initiative in the United Nations Environment Program (UNEP) has written a Guide explaining how to make a Social Life Cycle Assessment (S-LCA) of products (sees here). We take the aircraft as the product to be investigated in the S-LCA. Your task is:
1.) Review the state of the art of S-LCAs or Socio-Eco-Efficiency (SEE) related to Aircraft Design.
2.) Collect and select stakeholders, impact categories, indicators and related data as the basis for your proposed S-LCA.
3.) Build a spreadsheet as a support tool for an S-LCA for aircraft.
4.) Make an S-LCA for two different aircraft and draw your conclusions.
Hint: Aircraft noise should be one (of many) impact categories.
Projekt im Master Inland WS19-20
06.02.20
Helios
06.08.20 nein N-H V DS
Mehmet Öcalan Debunking Aeronautical Engineering Myths A fuel cell produces electricity with higher efficiency than a generator connected to the aircraft engine. Aircraft fly high to save on drag. SFC (Thrust Specific Fuel Consumption) is constant in a first order evaluation. Winglets improve wings. Wave drag is difficult to calculate. The drag coefficient starts to increases at Mach numbers beyond normal cruise speed. Aircraft should fly at their optimum speed which is quite high. An aircraft uses more fuel when it flies lower. Low Cost Airlines are the cause for additional fuel consumption and pollution. We have to reduce CO2 to save the world. The aviation industry does the utmost to save the world. --- Is it all true? Projekt Inland SS20
29.03.20
Helios
29.09.20 nein N-H   DS

 

Die folgenden Arbeiten wurden bereits abgegeben
eine 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
John Singh Cheema Der Massezuwachsfaktor - Schneeballeffekte im Flugzeugentwurf

Mass Growth and Reduction in Aircraft Design from Snowball Effects

"Aircraft undergoing a design process ... can encounter subsequent mass growth ... If the aircraft empty mass (OWE) increases, fuel consumption on a given (design) range rises. While increased fuel mass and volume may even require larger fuel tanks, it primarily results in a higher maximum take-off mass (MTOW) ..."

More in the dissertation by Risse on page 54 (PDF-page 88) in Chapter "3.1.4 Design interactions: mass snowball effect and aircraft resizing".

The mass snowball factor may have a value of 1.5.

This can already easily be shown with Equation 5.45 "First Law of Aircraft Design" as presented in Chapter 5 on http://hoou.profscholz.de (my Aircraft Design Lecture Notes).

The student is asked to start very easy with (5.45) and work towards a more detailed consideration of the Snowball Effects in Aircraft Design.

Projekt im Master Inland SS19
Helios
06.06.19
V 31.03.2020 nein N 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 N 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 N 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 N DS
Svenja Maaß Aircraft Recycling - A Literature Review RIBEIRO (2015) sees a "deficiency of knowledge and lack of total management for the aircraft life cycle from cradle to grave. Therefore, developing a conceptual framework for managing the end-of-life aircraft process is essential to achieving true sustainability". Today aircraft like the B787 and A350 are built with a higher percentage of CFRP and a lower percentage of metal. This saves weight and fuel, but causes problems at the end-of-life when disposal of carbon fibre components has to be managed. Start your review here http://doi.org/10.1016/j.procir.2014.07.048 und consider the Life Cycle Assessment as explained here: https://d-nb.info/1133261876/34 Project Inland WS19-20
28.10.19
Helios
28.04.19 nein N DS
Tobias Bähr, Sophie Sokour Calculating and Comparing Ecolabels for Popular Passenger Aircraft The task is to apply the definition and the rules to produce Ecolabels for Aircraft based on a) the work done already by other students and b) my presentation at the German Aerospace Conference 2017. See a) Task sheets to the Theses "Eco Lables for Aircraft" and "Definition of an Ecolabel for Aircraft". b) Presentation: "An Ecolabel for Aircraft". We want to calculate the data for the ecolabels for many popular passenger aircraft and compare and discuss the results. [Before we do all this, we have to fine tune the definition and design of the Ecolabel for Aircraft and have to compare and check the fuel consumption from two sources (Documents for Airport Planning and EEA)]. Project Inland WS17/18
14.11.17
Helios
14.05.18 nein J DS
Jascha McDavid Empennage Sizing - The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics *.pdf

We investigated the Tail Volume Coefficient already well (see Technical Note Ch. 2.5.2 and 3.1). What we need next is an evaluation and estimation of the lever arm measured from the wing to the tail in preliminary aircraft design. The lever arm is a percentage of the fuselage length. First hints are given in the lecture notes "Aircraft Design", Chapter 9. We need to rework the topic in more detail.

Project Inland SS17
25.04.17
Helios
V 25.11.17 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
Lynn Van Endert Definition of an Ecolabel for Aircraft Abstract: In attempting to increase the environmental awareness in the aviation sector and to eliminate the green washing phenomenon, an investigation was done into the development and definition of an ecolabel for aircraft. Based on life cycle assessment it was found that aviation affects the environment most with the impact categories resource depletion and global warming (both due to fuel consumption), local air pollution (due to the nitrogen oxide emissions in the vicinity of airports) and noise pollution. For each impact category a calculation method was developed based solely on official, certified and publicly available data to meet the stated requirements of the ISO standards about environmental labeling. To ensure that every parameter is evaluated independent on aircraft size, which allows comparison between different aircraft, normalizing factors such as number of seats, rated thrust and noise level limits are used. Additionally, a travel class weighting factor is derived in order to account for the space occupied per seat in first class, business class and economy class. To finalize the ecolabel, the overall environmental impact is determined by weighting the contribution of each impact category. For each category a rating scale from A to G is developed to compare the performance of the aircraft with that of others. The harmonization of the scientific and environmental information, presented in an easy understandable label, enables the traveling customers to make a well informed and educated choice when booking a flight, selecting among airline offers with different types of aircraft and seating arrangements. 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
Aday Pérez Reyes The Aviation Fuel and the Passenger Aircraft for the Future - Batteries Possibilities (or impossibilities) to operate an aircraft meeting requirements similar to an A320 with batteries and electrical motors. Master Thesis Ausland WS14/15
19.11.2014
E-Mail, Korn
02/2015 nein J DS
Leon Dib The Aviation Fuel and the Passenger Aircraft for the Future - Hydrogen Possibilities to operate an aircraft meeting requirements similar to an A320 with hydrogen Master Thesis Ausland WS14/15
19.11.2014
E-Mail, Korn
02/2015 nein J DS
Ramachandran Karunanidhi The Aviation Fuel and the Passenger Aircraft for the Future - Bio Fuel, Synthetic Fuel Analysis of the advantages and disadvantages of using alternative fuels in air transportation. Master Thesis Ausland WS14/15
19.11.2014
E-Mail, Korn
02/2015 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
Joeri Heinemann Preliminary Sizing - Part 25, Part 23, VLA and UL Aircraft *.pdf Master Thesis Ausland SS13 12.07.13 nein J 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:  12. 04. 2020
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
home  Fakultät Technik und Informatik
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