2026-09-24T06:13:11Z https://www.ideals.illinois.edu/oai-pmh

oai:www.ideals.illinois.edu:2142/113923 2023-07-11 col_2142_5131 col_2142_8888 com_2142_5130 com_2142_8887 com_2142_234

Haran, Kiruba S 2022-04-29T21:35:52Z 2021-12 Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2022-04-06 without embargo terms The student, Joshua Feldman, accepted the attached license on 2021-12-08 at 12:29. The student, Joshua Feldman, submitted this Thesis for approval on 2021-12-08 at 12:39. This Thesis was approved for publication on 2021-12-08 at 14:26. DSpace SAF Submission Ingestion Package generated from Vireo submission #17411 on 2022-04-06 at 17:11:09 Made available in DSpace on 2022-04-29T21:35:52Z (GMT). No. of bitstreams: 2 FELDMAN-THESIS-2021.pdf: 17635838 bytes, checksum: e46a32ad782e4bef0c0fcf1185ebca13 (MD5) LICENSE.txt: 4211 bytes, checksum: 17d7f993b5f9cc49d59e16d764f9af7b (MD5) Previous issue date: 2021-12-08 application/pdf en text Design and analysis of a cryogenic, liquid hydrogen based cooling system for a fully-superconducting aircraft propulsion motor Feldman, Joshua Michael 2021-12-08 Engineering 2022-04-29T21:35:52Z This thesis presents the design and modeling of a cooling system for a motor used for aircraft propulsion. The motivation behind this project lies in broader electric aircraft development efforts, and system requirements are presented as context for the research presented here. A design study is outlined, which includes a topology consideration and creation of an analytical thermal model. A design is presented with results of a thermal analysis showing the simulated performance of the design. Further work is also suggested. Thesis eng http://hdl.handle.net/2142/113923 Copyright 2021 Joshua Feldman Electrical & Computer Eng Electrical & Computer Engr University of Illinois at Urbana-Champaign Thesis M.S.