Preliminary sizing and optimization of propeller aircraft (Part 25)

Krull, Marlis; Scholz, Dieter

doi:10.48441/4427.2134

Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.2134

Publisher URL:	https://purl.org/aero/POS2024-09-30j https://publikationen.dglr.de/?tx_dglrpublications_pi1[document_id]=630513
Title:	Preliminary sizing and optimization of propeller aircraft (Part 25)
Language:	English
Authors:	Krull, Marlis Scholz, Dieter
Keywords:	Luftfahrt; Luftfahrzeug; Triebwerk; Propeller; Flugzeug; Flugtriebwerk; Turboluftstrahltriebwerk; Entwurf; Tabellenkalkulation; Optimierung; Aeronautics; Airplanes; Motors; Propellers; Spreadsheets; Design; Construction; Turbines; Mathematical optimization; Mach number; Engine; Aircraft; Sizing; Efficiency; ATR
Issue Date:	30-Sep-2024
Is supplemented by:	urn:nbn:de:gbv:18302-aero2022-04-29.012 10.7910/DVN/ET4ZKV
Conference:	Deutscher Luft- und Raumfahrtkongress 2024
Abstract:	Propeller driven aircraft have a higher propulsive efficiency, less drag, less Direct Operating Costs (DOC), and much less equivalent CO2 due to contrail avoidance at lower cruise altitude compared to traditional passenger jet aircraft. Accordingly, large propeller aircraft should be the choice for the next generation of aircraft to replace current passenger jets. For this reason, we teach such designs at HAW Hamburg based on our PhD-level research.
URI:	https://hdl.handle.net/20.500.12738/16687
DOI:	10.48441/4427.2134
Review status:	Currently there is no review planned for this version
Institute:	Forschungsgruppe Flugzeugentwurf und -systeme (AERO) Department Fahrzeugtechnik und Flugzeugbau Fakultät Technik und Informatik
Type:	Poster
Additional note:	KRULL, Marlis, SCHOLZ, Dieter, 2024. Preliminary Sizing and Optimization of Propeller Aircraft (Part 25). Poster. German Aerospace Congress (Hamburg, 30.09. - 02.10.2024). Available from: https://doi.org/10.48441/4427.2134
Appears in Collections:	Publications with full text