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Roto-Cycloid Propelled Airship Dimensioning and Energetic Equilibrium Universita di Modena e Reggio Emilia

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Trancossi, Trancossi, author.
Contributor:
Andrisani, Andrea
Dumas, Antonio
Pascoa, Jose
Xisto, Carlos
Conference Name:
SAE 2014 Aerospace Systems and Technology Conference (2014-09-23 : Cincinnati, Ohio, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2014
Summary:
AbstractRotocycloid propulsion presents interesting performance as a possible long-term alternative to helicopters in a far future. It will lead to increase the energy efficiency of VTOL vehicles. This paper focuses on optimization of an airship with the possibility up to 2000 h/year of photovoltaic propelled flight at a cruise speed about 20 m/s. This paper demonstrates the feasibility of this airship concept and presents a full dimensioning according to the CDE (Constructal Design for Efficiency) developed at University of Modena and Reggio Emilia. The proposed solution has been deeply analyzed and the analysis of performances has been presented. The results allow thinking to a novel class of vehicles designed specifically to take the maximum advantage by this propulsion method
Notes:
Vendor supplied data
Publisher Number:
2014-01-2107
Access Restriction:
Restricted for use by site license

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