TRANCOSSI, Michele, STEWART, Jill, MAHARSHI, Subhash and ANGELI, Diego (2016). Mathematical model of a constructal Coanda effect nozzle. Journal of Applied Fluid Mechanics, 9 (6), 2813-2822.
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Abstract
This paper analyses the ACHEON Coanda effect nozzle for aircraft propulsion, based on the dynamic equilibrium of two jet streams. The ACHEON concept, and, in particular, the HOMER nozzle, which is its main component, are presented, together with the literature milestones from which the idea originally stems. A subsystem analysis inspired by the principles of Constructal Theory is presented for the current architecture. A mathematical model of a 2D case of the system is developed, focusing on the combined effect of the mixing of the two streams and the Coanda adhesion over a convex surface. A validation of the model is also reported, based on 2D CFD analyses, under the hypothesis of incompressible flow. Results highlight that, in spite of its relative simplicity, the model produces accurate results.
Item Type: | Article |
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Uncontrolled Keywords: | Coanda effect; Fluid dynamic adhesion; Dual stream; Mathematical model; Constructal law. |
Research Institute, Centre or Group - Does NOT include content added after October 2018: | Materials and Engineering Research Institute > Engineering Research |
Page Range: | 2813-2822 |
Depositing User: | Michele Trancossi |
Date Deposited: | 08 Nov 2016 10:07 |
Last Modified: | 18 Mar 2021 06:01 |
URI: | https://shura.shu.ac.uk/id/eprint/13963 |
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Mathematical model of a constructal Coanda effect nozzle. (deposited 07 Sep 2016 09:03)
- Mathematical model of a constructal Coanda effect nozzle. (deposited 08 Nov 2016 10:07) [Currently Displayed]
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