Low Cost Narrow Body Aircraft

Bachelor Thesis (2016)
Author(s)

T.H.E. Gulikers (TU Delft - Aerospace Engineering)

D.W. van Hoogstraten (TU Delft - Aerospace Engineering)

R. Iordache (TU Delft - Aerospace Engineering)

I.C. Kleinbekman (TU Delft - Aerospace Engineering)

M.R. Koch (TU Delft - Aerospace Engineering)

D. Kroezen (TU Delft - Aerospace Engineering)

L. Müller (TU Delft - Aerospace Engineering)

M.M. Otting (TU Delft - Aerospace Engineering)

M.A. Pieters (TU Delft - Aerospace Engineering)

P. Proesmans (TU Delft - Aerospace Engineering)

Contributor(s)

Wim J.C. Verhagen – Mentor (TU Delft - Air Transport & Operations)

M Hernández Santana – Mentor (TU Delft - Novel Aerospace Materials)

Faculty
Aerospace Engineering
More Info
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Publication Year
2016
Language
English
Graduation Date
29-06-2016
Awarding Institution
Delft University of Technology
Project
AE3200 - Design Synthesis Exercise
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
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Abstract

As more and more people choose the airplane as a means of transportation, the aviation industry faces new challenges in order to fulfill the increasing demand, while decreasing the costs and emissions. In this report, the authors present a design of a narrow-body aircraft that is meant to provide a 30 % direct operating costs reduction, as well as a 20 % reduction in NOx and CO2 emissions while being ready for market introduction by 2030. Furthermore, the aircraft should provide a noise reduction of 10 % which translates to a reduction of 29 [EPNdB] and it should house 177 passengers.

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