Landing Gear Design Integration for the TU Delft Initiator

Master Thesis (2019)
Author(s)

Nick van Oene (TU Delft - Aerospace Engineering)

Contributor(s)

Roelof Vos – Mentor (TU Delft - Aerospace Engineering)

Vincent Brügemann – Graduation committee member (TU Delft - Aerospace Engineering)

Leo Veldhuis – Graduation committee member (TU Delft - Aerospace Engineering)

Faculty
Aerospace Engineering
More Info
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Publication Year
2019
Language
English
Graduation Date
07-03-2019
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
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Abstract

The Delft University of Technology is developing an MDO tool for the conceptual design of transport aircraft. However, the current program is not able to investigate the influence of the undercarriage design on the weight, drag and geometry of transport aircraft. This research proposes a new design method for the undercarriage, for which a new design module is created and integrated
into the Initiator architecture. This new method will allow the user to investigate the influence of the undercarriage design on the weight, drag and geometry transport aircraft concept.
By designing the undercarriage for six existing aircraft, it is shown that the updated Initiator is able to reliably and consistently design an undercarriage for a given transport aircraft concept. Also, two test cases demonstrate that the new method allows the user to evaluate the impact of the undercarriage on the drag, weight and geometry of the concept.

Files

Thesis_final_report.pdf
(pdf | 5.8 Mb)
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