Publisher URL: http://www.fzt.haw-hamburg.de/pers/Scholz/Indien/SCHOLZ-2016_PromisingConfigurationsForFuturePassengerAircraft_IDAD-Springer.pdf
http://India.ProfScholz.de
Publisher DOI: 10.1007/978-981-10-1771-1_1
Title: Promising Configurations for Future Passenger Aircraft
Language: English
Authors: Scholz, Dieter  
Editor: Bajpai, Ram P. 
Chandrasekhar, U. 
Keywords: 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
Issue Date: 2017
Publisher: Singapor ; Springer
Book title: Innovative design and development practices in aerospace and automotive engineering
Part of Series: Lecture notes in mechanical engineering 
Startpage: 1
Endpage: 3
Conference: International Conference on Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering 2016 
Abstract: 
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
Institute: Department Fahrzeugtechnik und Flugzeugbau 
Fakultät Technik und Informatik 
Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Type: Chapter (Book)
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