Afterburning of High-Temperature Products of Incomplete Combustion in a Supersonic Flow upon a Secondary Injection of Oxidizer,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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The article is an examination of the results of an experimental study in the afterburning of a supersonic flow of products that have not completely burned on account of re-injected oxidizers HNO3 and N2O4.
- Combustion and Ignition