New approach to ramjet design suitable for very high speed flight developed by Armstrong Whitworth Aircraft; principle of study is that of spontaneous ignition of fuel by shock heating; this would make it unnecessary to slow internal flow to subsonic values, hence eliminate flame holders; way of obtaining multi-shock compression is explained; eight sided duct is needed to give 8-stage shock compression, requirement for good pressure recovery around Mach 5 or 6; flow characteristics of flat sided venturi configurations.
Diesel ramjet design
Aircraft Missiles
Aircraft and Missiles ; 3 , n 5 ; p 50-51
1960
2 pages
Article (Journal)
English
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