Basic Comparison of Three Aircraft Concepts: Classic Jet Propulsion, Turbo-Electric Propulsion and Turbo-Hydraulic Propulsion
Purpose - This thesis presents a comparison of aircraft design concepts to identify the superior propulsion system model among turbo-hydraulic, turbo-electric and classic jet propulsion with respect to Direct Operating Costs (DOC), environmental impact and fuel burn. --- Approach - A simple aircraf...
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Format: | Others |
Language: | English |
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Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences,
2019
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Online Access: | http://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-09-22.014 http://doi.org/10.15488/9329 http://n2t.net/ark:13960/t2k72zp1t http://d-nb.info/1204558019 http://library.ProfScholz.de http://www.fzt.haw-hamburg.de/pers/Scholz/arbeiten/TextRodrigo.pdf http://www.fzt.haw-hamburg.de/pers/Scholz/arbeiten/TextRodrigo.jpg http://doi.org/10.7910/DVN/K5FLHR |
Internet
http://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2019-09-22.014http://doi.org/10.15488/9329
http://n2t.net/ark:13960/t2k72zp1t
http://d-nb.info/1204558019
http://library.ProfScholz.de
http://www.fzt.haw-hamburg.de/pers/Scholz/arbeiten/TextRodrigo.pdf
http://www.fzt.haw-hamburg.de/pers/Scholz/arbeiten/TextRodrigo.jpg
http://doi.org/10.7910/DVN/K5FLHR