Digital Library - Projects & Theses

Aircraft Design, Flicht Mechanics, Aircraft Systems. --- This dataverse contains research data and software produced by students for their projects and theses. --- Get linked to all other resources from their reports using the URN from the German National Library (DNB) as given in each dataset under "Metadata".

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1,391 to 1,400 of 1,453 Results

iopn_trajectory.obj Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process TGIF File - 62.7 KB - MD5: beb7bdebe72d87c45f65ab92160d3631
Sphere Net.dsp Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process Unknown - 3.6 KB - MD5: 75907d777a370e91cac9f7928aca7b9e
Sphere Net.dsw Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process Unknown - 545 B - MD5: 64a73979d567ea1bc03cc90c705ee270
Sphere Net.exe Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process Windows Executable - 280.0 KB - MD5: 518d7c79691c85f991d5805dd79fc0c5
Sphere Net.f90 Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process Fortran Source Code - 6.4 KB - MD5: dc405122cd049b8417842b4025c720e7
Sphere Net.obj Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process TGIF File - 10.5 KB - MD5: ce6145023aa2189e6dcbe019fa32d492
V_IOPANAM.txt Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process Plain Text - 13.3 KB - MD5: d9c90c3cd428a909f18419f645a54217
Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics May 15, 2021 McDavid, Jascha; Kühner, Benjamin, 2021, "Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics", https://doi.org/10.7910/DVN/TLFDIU, Harvard Dataverse, V1 This project gives an overview of a selection of geometrical parameters with respect to the tail volume coefficient. A statistic on the basis of 30 aircraft, which differ in their dimensions, was made. One target was to create a graphical method for finding the tail levers arms, both for the horizontal, and the vertical tail. The average tail lever...
Statistics.xls May 15, 2021 - Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics MS Excel Spreadsheet - 147.5 KB - MD5: a5e588b346f3186dd53fa019d9d28ea6
Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing Apr 7, 2021 Gmelin, Philipp, 2021, "Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing", https://doi.org/10.7910/DVN/NKTCX1, Harvard Dataverse, V1, UNF:6:6rLNFZ4iIbdoTijJwE7KYw== [fileUNF] The purpose of this project is to examine and describe the regulations of microlight aircraft. The national rules of mostly European countries are described in more detail and are compared to the German rules. Most important among the regulations is the maximum take-off mass. In some countries, the limit of 472.5 kg has been raised recently to 600...

iopn_trajectory.obj

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

TGIF File - 62.7 KB -

Sphere Net.dsp

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

Unknown - 3.6 KB -

Sphere Net.dsw

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

Unknown - 545 B -

Sphere Net.exe

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

Windows Executable - 280.0 KB -

Sphere Net.f90

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

Fortran Source Code - 6.4 KB -

Sphere Net.obj

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

TGIF File - 10.5 KB -

V_IOPANAM.txt

Jun 5, 2021 - Integration of a Noise Analysis Module into a Multidisciplinary Aircraft Design Process

Plain Text - 13.3 KB -

Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics

May 15, 2021

McDavid, Jascha; Kühner, Benjamin, 2021, "Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics", https://doi.org/10.7910/DVN/TLFDIU, Harvard Dataverse, V1

This project gives an overview of a selection of geometrical parameters with respect to the tail volume coefficient. A statistic on the basis of 30 aircraft, which differ in their dimensions, was made. One target was to create a graphical method for finding the tail levers arms, both for the horizontal, and the vertical tail. The average tail lever...

Statistics.xls

May 15, 2021 - Empennage Sizing: The Tail Lever Arm as a Percentage of Fuselage Length Determined from Statistics

MS Excel Spreadsheet - 147.5 KB -

Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing

Apr 7, 2021

Gmelin, Philipp, 2021, "Requirements from National Regulations for Microlight Aircraft and Statistical Parameters for Preliminary Sizing", https://doi.org/10.7910/DVN/NKTCX1, Harvard Dataverse, V1, UNF:6:6rLNFZ4iIbdoTijJwE7KYw== [fileUNF]

The purpose of this project is to examine and describe the regulations of microlight aircraft. The national rules of mostly European countries are described in more detail and are compared to the German rules. Most important among the regulations is the maximum take-off mass. In some countries, the limit of 472.5 kg has been raised recently to 600...

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