SPH numerical investigation of the velocity field and vorticity generation within a hydrofoil-induced spilling breaker

2015 ◽  
Vol 16 (1) ◽  
pp. 267-287 ◽  
Author(s):  
Diana De Padova ◽  
Michele Mossa ◽  
Stefano Sibilla
Author(s):  
Virginia Fratalocchi ◽  
Jim B. W. Kok

A numerical investigation of the interaction between a spray flame and an acoustic forcing of the velocity field is presented in this paper. The test-case which is the focus of this work is a non-confined flame1,2 burning at atmospheric pressure and therefore the velocity fluctuations play a key role. Acoustic waves will eventually affect the rate of combustion, and the oscillating fluctuation of the heat released by the flame might be increased by the evaporation process. The dynamic interaction between the evaporating fuel spray and the velocity fluctuations induced by an acoustic perturbation is investigated to understand the impact of the acoustic waves on the droplet dispersion and on the evaporation rate. The influence of the initial droplet diameter has been observed to be irrelevant, when two monodispersed sprays of 20 μm and 80 μm were numerically simulated. In this work the main question to address is how the interphase heat and mass transfer, and the momentum exchange are influenced, at low amplitude velocity fluctuations, by the forcing frequency, under two different imposed velocity profiles of the liquid fuel. A fast decay of the slip velocity is predicted under both steady and perturbed conditions. Thus, slip velocity fluctuations do not have a significant influence on the solved spray field. Finally, the impact of the forcing frequency and of the pilot are the main effects acting on the forced flame response. At low frequency, the entrainment of hot gases into the spray results in a clearly visible stretching of the flame which causes a high level of temperature fluctuation. At high frequency, despite the weak response of the gas velocity field, the dynamics of the combustion show a faster evaporation rate than the acoustic–free case.


Author(s):  
Ivan A. Anchondo ◽  
Ahsan R. Choudhuri

This paper presents a numerical investigation of the mixing of methane and air inside a 5mm high and 40 mm long 2-D channel type microcombustor. Two fuel-air injection schemes are studied at different equivalence ratios. Configuration-I injects methane from an axially located port, whereas configuration-II injects methane from two radially located opposing ports. The velocity field and local methane mixture fractions indicate that the configuration-I provides a superior mixing for lean, stoichiometric and rich equivalence ratios. However, configuration-II yields sufficient mixing only at a fuel rich condition. Also, despite geometrical symmetry of the chamber, flow-fields are highly asymmetric at a lean condition in both configurations.


2013 ◽  
Vol 401-403 ◽  
pp. 214-217
Author(s):  
Ping Wang ◽  
Yong Ze Li ◽  
Bo Sun ◽  
Hui Guo ◽  
Yu Chen

Method of CFD is used in this paper to simulate and calculate velocity field, temperature field and droplet track in PCZ(primary combustion zone) under the 3D two phase turbulent combustion for the ground idling, the peak, the middling and the altitude-small lever flying conditions. By analyzing the calculation results and comparing with tests, characters of PCZ are well investigated.


1964 ◽  
Vol 86 (4) ◽  
pp. 845-850 ◽  
Author(s):  
E. J. Rodgers

An experimentally obtained velocity field about a body of revolution at a small angle of attack, and at subsonic velocity, is used to determine the vorticity distribution about the body. Surface-flow visualization and pressure-distribution tests are used to supplement the vorticity-distribution data in attempting to explain the mechanisms of the flow, and thus the differences between the real flow and that predicted by potential theory.


2012 ◽  
Vol 9 (4) ◽  
pp. 511-520 ◽  
Author(s):  
Reza Maddahian ◽  
Mohammad Asadi ◽  
Bijan Farhanieh

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