Landing Gear Design Integration for the TU Delft Initiator

Master thesis (2019)

Authors

N. van Oene Aerospace Engineering

Contributors

Roelof Vos Flight Performance and Propulsion - Aerospace Engineering (supervisor 1)
V.P. Brügemann Structural Integrity & Composites - Aerospace Engineering (supervisor 2)
L.L.M. Veldhuis Flight Performance and Propulsion - Aerospace Engineering (supervisor 2)
Faculty
Aerospace Engineering
Copyright: © 2019 Nick van Oene
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Published Date

07-03-2019

Language

English

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Faculty

Aerospace Engineering

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.