On recessed cavity flame-holders in supersonic cross-flows

On recessed cavity flame-holders in supersonic cross-flows

Flame-holding in a recessed cavity is investigated experimentally in a Mach 2.5 preheated cross-flow for both stable and unstable combustion, with a relatively low preheating. Self-sustained combustion is investigated for stagnation pressures and temperatures reaching 1.4 MPa and 750 K. In particula...

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Bibliographic Details
Main Author: Retaureau, Ghislain J.
Published: Georgia Institute of Technology 2012
Subjects:
Risk
Hypersonic
Scramjet
Propulsion
Shock
Heat transfer
Compressible flow
Wind tunnel design
Ignition delay
Residence time
Nozzle
Interpolation
Propulsion systems
Combustion
Flame stability
Online Access:http://hdl.handle.net/1853/43703

Internet

http://hdl.handle.net/1853/43703

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