Print Email Facebook Twitter Aerodynamic Design and Optimization of a Hyperloop Vehicle Title Aerodynamic Design and Optimization of a Hyperloop Vehicle Author Wong, Felix (TU Delft Aerospace Engineering) Contributor van Zuijlen, A.H. (mentor) Veldhuis, L.L.M. (graduation committee) Voskuijl, M. (graduation committee) van der Meijs, Marinus (graduation committee) Degree granting institution Delft University of Technology Programme Aerospace Engineering Date 2018-05-23 Abstract The Hyperloop is a newly proposed transportation method which caters to the rising demand of high-speed transportation, while adhering to stringent emission requirements. This system comprises pods that are propelled through a partially evacuated tube at velocities of 300 m/s. The low-pressure environment paired with high-subsonic Mach numbers create an unconventional flow regime. This thesis project is an investigation on the aerodynamic characteristics of a Hyperloop pod, whereby an optimization is performed in order to find a pod shape that yields minimum drag. A low-fidelity solver is developed to perform the analysis and optimization. Investigations show a large pressure peak at the nose due to violation of the Kantrowitz limit. Furthermore, a blunt nose paired with a concavity in the tail section yield minimum drag due to the alleviation of the choked flow effect. The solver can readily be embodied into a larger, multi-disciplinary optimization framework. Subject AerodynamicDesignHyperloop To reference this document use: http://resolver.tudelft.nl/uuid:b91cbd15-3f0b-4491-ae49-fdc01854927c Part of collection Student theses Document type master thesis Rights © 2018 Felix Wong Files PDF MSc_Thesis_Report_Felix_Wong.pdf 14.98 MB Close viewer /islandora/object/uuid:b91cbd15-3f0b-4491-ae49-fdc01854927c/datastream/OBJ/view