Numerical analysis of rotating ramps in a scramjet engine

dc.contributor.authorLiang, J.
dc.contributor.authorWei, H.
dc.contributor.authorZhen, L.
dc.contributor.authorJun, L.
dc.date.accessioned2015-04-23T07:00:33Z
dc.date.available2015-04-23T07:00:33Z
dc.date.issued2014
dc.description.abstractPaper presented to the 10th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, Florida, 14-16 July 2014.en_ZA
dc.description.abstractA concept of mixing enhancement forced by rotating ramps has been presented, which based on the design of stationary ramps and Rim-Rotor Rotary Ramjet Engine. The rotating ramps could generate large scale vortex and rotary moving shock waves, which may increase the fuel mixing rate and spread distance in transverse-direction. The commercial software Fluent has been conducted to study the effect of different velocity of ramps rotating on flowfield characteristics. The results show that rotating ramps increase the periodic oscillation of cavity shear layer and induce large streamwise vortices in cavity. When the ramps rotate at a speed of 54.3krpm, the peak value of x-vortex magnitude is nearly four times as the stationary ramps, however, the coefficient of total pressure recovery in the rotating ramps case is nearly 10% less than that in the stationary ramps case. This study provides a new method for mixing enhancement under supersonic airflow condition.en_ZA
dc.description.librariandc2015en_ZA
dc.format.extent6 pagesen_ZA
dc.format.mediumPDFen_ZA
dc.identifier.citationLiang, J, Wei, H, Zhen, L & Jun, L 2014, 'Numerical analysis of rotating ramps in a scramjet engine', Paper presented to the 10th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, Florida, 14-16 July 2014.en_ZA
dc.identifier.isbn97817759206873
dc.identifier.urihttp://hdl.handle.net/2263/44486
dc.publisherInternational Conference on Heat Transfer, Fluid Mechanics and Thermodynamicsen_ZA
dc.rights© 2014 University of Pretoria. All rights reserved. The copyright in this work vests in the University of Pretoria. No part of this work may be reproduced or transmitted in any form or by any means, without the prior written permission of the University of Pretoria.en_ZA
dc.subjectMixing enhancementen_ZA
dc.subjectRotating rampsen_ZA
dc.subjectRim-Rotor Rotary Ramjet Engineen_ZA
dc.subjectRotary moving shock wavesen_ZA
dc.subjectSupersonic airflow conditionen_ZA
dc.titleNumerical analysis of rotating ramps in a scramjet engineen_ZA
dc.typePresentationen_ZA

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