Landing Gear Design Integration for the TU Delft Initiator

Title

Landing Gear Design Integration for the TU Delft Initiator

 Author

van Oene, Nick (TU Delft Aerospace Engineering)

Contributor

Vos, Roelof (mentor)
Brügemann, Vincent (graduation committee)
Veldhuis, Leo (graduation committee)

Degree granting institution

Delft University of Technology

 Programme

Aerospace Engineering

 Date

2019-03-07

 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.

 Subject

Landing gear
Undercarriage
Concept Design
MDO
Initiator
optimization

 To reference this document use:

http://resolver.tudelft.nl/uuid:e08c31c2-1371-465d-a5bc-666433945249

 Part of collection

Student theses

 Document type

master thesis

 Rights

© 2019 Nick van Oene
Files
PDF Thesis_final_report.pdf 5.8 MB
Close viewer