Verlagslink: http://www.fzt.haw-hamburg.de/pers/Scholz/Indien/SCHOLZ-2016_PromisingConfigurationsForFuturePassengerAircraft_IDAD-Springer.pdf
http://India.ProfScholz.de
Verlagslink DOI: 10.1007/978-981-10-1771-1_1
Titel: Promising Configurations for Future Passenger Aircraft
Sprache: Englisch
Autorenschaft: Scholz, Dieter  
Herausgeber*In: Bajpai, Ram P. 
Chandrasekhar, U. 
Schlagwörter: Passenger aircraft; Payload; Cargo; Hydrogen tank; Synthetic fuel; Drop-in fuel; Turboprop; Braced wing; Natural laminar flow; High aspect ratio; Span; Battery; Hydrogen; Stretch; Synthetic fue
Erscheinungsdatum: 2017
Verlag: Singapor ; Springer
Buchtitel: Innovative design and development practices in aerospace and automotive engineering
Teil der Schriftenreihe: Lecture notes in mechanical engineering 
Anfangsseite: 1
Endseite: 3
Konferenz: International Conference on Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering 2016 
Zusammenfassung: 
A promising aircraft configuration for typical short to medium range would be a turboprop aircraft with large propeller diameter. The concept can benefit further from a strut braced wing and natural laminar flow. Most important for an efficient aircraft design is a high aspect ratio. For a given span (limits at airports need to be observed) the effective aspect ratio can be increased with winglets or folding wings. Much better would be to offer wing tip extensions to standard aircraft, accepting the next larger ICAO wing span category for some aircraft in the fleet. Electric flight on batteries is not the answer due to severe range limitations. Regenerative energy could be converted to hydrogen with electrolysis and stored as liquid hydrogen (LH2) in a stretched fuselage with hydrogen tanks installed in front and aft of the cabin. Research is on the way to directly convert (regenerative electrical) energy to hydrocarbons. Such synthetic fuel could be used even in older aircraft offering a fast improvement for the environment.
URI: http://hdl.handle.net/20.500.12738/273
ISBN: 978-981-10-1770-4
978-981-10-1771-1
Einrichtung: Department Fahrzeugtechnik und Flugzeugbau 
Fakultät Technik und Informatik 
Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Dokumenttyp: Kapitel (Buch)
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