TI3115TU Report Template
Report template for students of TU Delft's course TI3115TU Software Engineering and Methods, part of the Minor Computer Science.
Maurício Aniche, Georgios Andreadis
Template for TU Delft Reports-Theses
This is the TU Delft LaTeX template for reports and theses, downloaded from TU Delft corporate design downloads. The template is designed to work with all versions of LaTeX, but if you want to adhere to the TU Delft house style, you need to use XeLaTeX, as it supports TrueType and OpenType fonts.
Template for TU Delft Dissertation
This is the TU Delft LaTeX template for dissertations, downloaded from TU Delft corporate design downloads.
The template is designed to
work with all versions of LaTeX, but if you want to adhere to the TU Delft house
style, you need to use XeLaTeX, as it supports TrueType and OpenType fonts.
TU Delft (uploaded by LianTze Lim)
MSc Geomatics Thesis Template - TU Delft
A complete template for the MSc Geomatics thesis.
It contains all the parts that are required and is structured in such a way that most/all supervisors expect. Observe that the MSc Geomatics at TU Delft has no formal requirements, how the document looks like (fonts, margins, headers, etc) is entirely up to you. We basically took the template arsclassica (by Lorenzo Pantieri), which is an adaption of the original `classicthesis package from André Miede, added the front/back matters (cover page, copyright, abstract, etc.), and gave examples for the insertion of figures, tables and algorithms.
test simulation plan
This simulation plan aims to explain and document all steps to be taken in the simulation
analysis of the Fokker-100 case. This case is the scenario in which the aircraft touches the
ground during landing, introducing loads on the landing gear. The landing gear consists of
2 rear gears around mid-span and one in the front. Furthermore, the pilot uses the rudder
which induces a lateral force on the tail.
As stated in the assignment, it is required to find the maximum normal stress and location
of this in the fuselage, the maximum shear stress and its location in the fuselage, and the
flow in the frames that introduce the loads from the landing gears into the