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Journal ArticleDOI

Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

Adela Ben-Yakar, +1 more
- 01 Jan 2001 - 
- Vol. 17, Iss: 4, pp 869-877
TLDR
In this article, the authors describe ongoing research efforts in the scramjet community on cavity e ame holders, a concept for holding and stabilization in supersonic combustors, and discuss open questions impacting the effectiveness of the cavities as a holding device.
Abstract
This paper describes ongoing research efforts in the scramjet community on cavity e ame holders, a concept for e ame holding and stabilization in supersonic combustors. During the last few years, cavities have gained the attention of the scramjet community as a promising e ame-holding device, owing to results obtained in e ight tests and to feasibility demonstrations in laboratory-scale supersonic combustors. However, comprehensive studies are needed to determine the optimal cone guration that will yield the most effective e ame-holding capability with minimum losses. The e owe eld characteristics of cavities and research efforts related to cavities employed in lowand high-speed e ows are summarized. Open questions impacting the effectiveness of the cavities as e ame holders in supersonic combustors are discussed.

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Citations
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Journal ArticleDOI

Mixing and combustion studies using cavity-based flameholders in a supersonic flow

TL;DR: In this article, an experimental investigation of the mixing and combustion processes that occur in and around a cavity-based flameholder in a supersonic flow is reported, which is part of an ongoing research program aimed at providing information to help fill these voids and improve the overall understanding of cavities for use as scramjet flameholders.
Journal ArticleDOI

Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder

TL;DR: In this paper, the combustion characteristics of a laboratory dual-mode ramjet/scramjet combustor were studied experimentally, and two distinct combustion stabilization locations were found for fuel injection a sufficient distance upstream of the cavity.
Journal ArticleDOI

Applications of quantitative laser sensors to kinetics, propulsion and practical energy systems

TL;DR: In this article, the authors highlight three areas where quantitative sensing based on laser absorption has had strong influence: chemical kinetics, propulsion, and practical energy systems, and provide an overview of the current power and future potential of these modern diagnostic tools.
Journal ArticleDOI

Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor

TL;DR: In this paper, the authors investigated the characteristics of cavity assisted hydrogen jet combustion in a supersonic flow with a total pressure of 1.6 MPa, a total temperature of 1486 K, and a Mach number of 2.52, simulating flight Mach 6 conditions.
Journal ArticleDOI

A review of cavity-based trapped vortex, ultra-compact, high-g, inter-turbine combustors

TL;DR: Trapped vortex combustion (TVC) as mentioned in this paper is a promising combustion concept that has been extensively studied in the application areas of aerospace propulsion, power generation and waste incineration, where a large rotating vortex can be formed in the cavity and is thus named a locked vortex.
References
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Journal ArticleDOI

The compressible turbulent shear layer: an experimental study

TL;DR: In this paper, the growth rate and turbulent structure of the compressible, plane shear layer are investigated experimentally in a novel facility, where it is possible to flow similar or dissimilar gases of different densities and to select different Mach numbers for each stream.
Journal ArticleDOI

Flow-Induced Pressure Oscillations in Shallow Cavities

TL;DR: In this paper, the results of an experimental wind-tunnel study of flow-induced pressure oscillations in shallow cavities (length-to-depth ratio from 4 to 7) were presented.
Journal ArticleDOI

Research on supersonic combustion

TL;DR: In this article, the authors present a design model that is based on the use of integral techniques to describe combustion in supersonic flow from experiments conducted in an arc-heated tunnel.
Journal ArticleDOI

Characteristics of a Trapped-Vortex Combustor

TL;DR: In this article, the characteristics of a trapped-vortex (TV) combustor are described and the instantaneous shape of the recirculation zone of the trapped vortex is measured using a two-color PIV technique.
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