ACHEON numerical modeling presented at Multiphysics 2013

In the framework of the conference Multiphysics 2013 that is going to take place in Amsterdam on 12-13 December 2013. Dr. Shyam Das, researcher at UBI, will be briefing about the ongoing research on “Numerical modeling of Coanda effect in a Novel Propulsive System”. The cooperative research of the WP3 Team members resulted in a […]

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Keynote Lecture at the Eleventh International Conference of Fluid Dynamics (ICFD 11)

On 19-21 December  2013, Prof. Dean Vucinic (VUB) is invited as keynote speaker at the Eleventh International Conference of Fluid Dynamics (ICFD 11).  The keynote lecture will focus on  “CFD as the essential engineering tool in the European MAAT and ACHEON projects” [Lecture/Paper number: ICFD11-EG-40I08]. The conference will be held in Aleksandria, Egypt. For more information go to http://www.icfd11.org. […]

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ACHEON unveiled at ASME IMECE 2013

UNIMORE will present a paper on “MATHEMATICAL MODELLING OF A TWO STREAMS COANDA EFFECT NOZZLE” at IMECE 2013 – ASME International Mechanical Engineering Congress and Exposition November 15-21, San Diego, CA, USA [Paper N° IMECE2013-63459]. At ASME you can meet the consortium delegates to discuss future cooperation for greening the air transport and to plan […]

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Computational Study of the Coanda Flow Using the K-zeta-f Turbulence Model at CAE

UNIMORE will present a paper on Computational Study of the Coanda Flow Using the K-zeta-f Turbulence Model at CAE International Conference – Areospace & defense session 22 Oct 2013, Pacengo sul Garda (IT). CAE is one of the most important forum for Computational and Simulation Technologies. http://www.caeconference.com/abstract/unimo.html   Bookmark It Hide Sites

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ACHEON papers published online in SAE Technical Papers

The ACHEON papers presented at SAE Aerotech2013 are published as SAE Technical Papers. Check out our latest foreground on Coanda based thrust vectoring technology for green the air transport at www.sae.org 1.       Maharshi S.,  and Dumas, A., “Computational Study of Coanda Adhesion Over Curved Surface,” SAE Int. J. Aerosp. 6(1):260-272, 2013, doi:10.4271/2013-01-2302. [Related to WP3] […]

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Paper presented at ATI on “The Influence of Surface temperature on Coanda Surface”

UNIMORE presented a paper on “The Influence of Surface Temperature on Coanda Surface” at  68° Congresso Nazionale Associazione Termotecnica Italiana (ATI). The congress took place in Bologna on 11-13 September 2013. The paper presented is expected to be published in Energy Procedia – an Elsevier Journal. Bookmark It Hide Sites

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Online the ACHEON Scientific Project Presentation

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The UBI Team of Prof J. Pascoa published a multimedia scientific presentation to illustrate the FP7 ACHEON project challenges, its experimental methodology and the future disruptive impact arising from the demonstration of the scientific feasibility of a Coanda-based thrust vectoring technology with no mechanical moving parts. To enjoy the presentation clicki here.   Bookmark It […]

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Animations showcasing the ACHEON HOMER nozzle

UBI released 3 multimedia animations illustrating the conceptual design of the HOMER nozzle and the guided vanes near inlet section. Ongoing 3D CFD Studies (Das and Pascoa, 2013) shows that the flows are not completely axial, thus the tangential component of the flow field can’t be neglected. Guided vanes were proposed for reducing the swirling […]

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Online the ACHEON Newsletter N°1

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The newsletter highlights the interim research results achieved and the latest papers published by the ACHEON Consortium during the first nine months of the project activities. It also reports about the main scientific and technological events and fora where is possible to meet the Consortium Members in order to discuss the actions necessary to move from […]

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Preliminary CFD analysis and Technology Evaluation Accomplished

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The Acheon Consortium released the deliverables about the preliminary CFD analysis (UNiMORE & UBI) and the Technology Evaluation (UoL). The deliverable are available for third parties upon written request.   Velocity contours for Vav = 35m-s showing the different angle for different velocity ratio   Bookmark It Hide Sites

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