A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation

Author:

Trancossi Michele,Madonia Mauro,Dumas Antonio,Angeli Diego,Bingham Chris,Das Shyam Sumanta,Grimaccia Francesco,Marques Jose Pascoa,Porreca Eliana,Smith Tim,Stewart Paul,Subhash Maharshi,Sunol Anna,Vucinic Dean

Funder

Seventh Framework Programme (BE)

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Transportation,Automotive Engineering

Reference51 articles.

1. Sehra AK (2003) Novel propulsion and power concepts for 21st century aviation. AVT Spring 2003 Symposium and Panel Business Week, Brussels

2. Trancossi M, Dumas A (2011) ACHEON: Aerial Coanda high efficiency orienting-jet nozzle. Sae Technical Papers N. 2011-01-2737, ISSN 0148–7191

3. Cen Z, Smith T, Stewart P, and Stewart J. Integrated flight/thrust vectoring control for jet-powered unmanned aerial vehicles with ACHEON propulsion. Proc Inst Mech Eng Part G: J Aerospace Eng 0954410014544179, first published on July 29, 2014 doi: 10.1177/0954410014544179

4. Trancossi M (2011) An overview of scientific and technical literature on coanda effect applied to nozzles. SAE Technical Papers N. 2011-01-2591, ISSN 0148–7191

5. Baffigi F, Dumas A, Giuliani I, Madonia M, Trancossi M (2014) Ugello capace di deviare in modo dinamico e controllabile un getto sintetico senza parti meccaniche in movimento e relativo sistema di controllo. Patent IT 0001406404, Deposito RE2011A000049, Filling date July 01, 2011, Publication date September 30, 2011, approved on February 21, 2014

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