Publication Date:
2019-06-27
Description:
The use of heat conduction flame generated in a premixed supersonic stream is discussed. It is shown that the flame is controlled initially by heat conduction and then by chemical reaction. Such a flame is shorter than the diffusion type of flame and therefore it requires a much shorter burner. The mixing is obtained by injecting the hydrogen in the inlet. Then the inlet can be cooled by film cooling.
Keywords:
PROPULSION SYSTEMS
Type:
NASA-CR-132446
Format:
application/pdf