Journal ArticleDOI
Numerical study on supersonic combustion with cavity-based fuel injection
TLDR
In this article, the authors describe the numerical investigations concerning the combustion enhancement when a cavity is used for the hydrogen fuel injection through a transverse slot nozzle into a supersonic hot air stream.About:
This article is published in International Journal of Heat and Mass Transfer.The article was published on 2004-01-01. It has received 196 citations till now. The article focuses on the topics: Combustor & Combustion.read more
Citations
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Journal ArticleDOI
Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows
TL;DR: In this article, the effect of the turbulence model and slot width on the transverse slot injection flow field has been investigated numerically based on the grid independency analysis, and the predicted results have been compared with the experimental data available in the open literature.
Journal ArticleDOI
Plasma assisted cavity flame ignition in supersonic flows
TL;DR: In this article, a nanosecond pulsed plasma discharge located within a wall cavity is used to ignite jet flames (hydrogen and ethylene) in supersonic crossflows.
Journal ArticleDOI
Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity
TL;DR: In this article, a large eddy simulation (LES) was carried out to investigate a hydrogen-fueled scramjet combustor with dual cavity, where a Reynolds-Averaged Navier-Stokes (RANS) model was used for near-wall treatment.
Journal ArticleDOI
Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows
TL;DR: In this article, the effect of the swept angle, the ramp angle and the length of the step on the performance of the cantilevered ramp injector has been investigated numerically, and the predicted injectant mole fraction and static pressure profiles have been compared with the available experimental data in the open literature.
Journal ArticleDOI
Flame propagation and stabilization in dual-mode scramjet combustors: A survey
TL;DR: In this paper, the authors reviewed and summarized the research progress on the flame propagation and stabilization in the dual-mode scramjet combustor, and their main focus is on the mode transition.
References
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Proceedings ArticleDOI
Thin-layer approximation and algebraic model for separated turbulent flows
B. Baldwin,H. Lomax +1 more
TL;DR: In this article, an algebraic turbulence model for two-and three-dimensional separated flows is specified that avoids the necessity for finding the edge of the boundary layer, and compared with experiment for an incident shock on a flat plate, separated flow over a compression corner, and transonic flow over an airfoil.
Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications II. Users Manual and Program Description. 2; Users Manual and Program Description
Bonnie J. McBride,Sanford Gordon +1 more
Journal ArticleDOI
A Viscosity Equation for Gas Mixtures
TL;DR: In this paper, the previous equation of Buddenberg and the author has been modified to give a general equation for viscosity as a function of molecular weights and viscosities of the pure components of the mixture.
Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations
Sanford Gordon,Bonnie J. McBride +1 more
TL;DR: Computer program is described for numerical solution of chemical equilibria in complex systems by using nonlinear algebraic equations using free-energy minimization technique.
Related Papers (5)
Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
Adela Ben-Yakar,Ronald K. Hanson +1 more