| 摘要 |
A combustion process derived from boundary layer stream containment and manipulation of all the combustion phases in auto-pro-progression, within a unitary-continuous sequence, in a supersonic and/or high subsonic velocity mainstream employs no auxiliary devices, systems, phases, streams or fuels and introduces novel means for generating and sustaining the process, using common fuels. It is applicable to stationary power and high thrust propulsion sources.
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