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Flow Studies on a Hydrogen-Fueled Cavity Flame-Holder Scramjet

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Date

2005

Authors

Neely, Andrew
Stotz, Ingo
O'Byrne, Sean
Boyce, Russell R
Mudford, Neil
Houwing, A Frank

Journal Title

Journal ISSN

Volume Title

Publisher

American Institute of Aeronautics and Astronautics

Abstract

This work extends an investigation into the use of a cavity flameholder to aid scramjet combustion at high flight Mach number. A parallel scramjet duct incorporating a cavity flame holder in the floor with an inclined rear face and an aspect ratio of 4.8

Description

Keywords

Keywords: Cavity flame holders; Mach number; Scramjets; Shock tunnels; Aspect ratio; Combustion; Computational fluid dynamics; Computer simulation; Flight dynamics; Fluorescence; Hydrogen fuels; Laser beams; Jets

Citation

URI

http://hdl.handle.net/1885/83626

Collections

ANU Research Publications

Source

OH PLIF Imaging of Supersonic Combustion Using Cavity Injection

Type

Conference paper

Book Title

Entity type

Access Statement

License Rights

DOI

Restricted until

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