Investigation of the 3-D Hydrogen Flame Structure in a Supersonic High-Temperature Air Flow by Optical Methods
RUSSIAN ACADEMY OF SCIENCES NOVOSIBIRSK INST OF THEORETICAL AND APPLIED MECHANICS
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In this work the experimental results of research of a plume structure at axial hydrogen injection in a supersonic high-temperature air jet are presented. Two levels of temperatures are compared. One of them 1500-2000 K is usually achieved in the ground experimental facility with a long period of action. The other level of temperature 2500-2700 K is characteristic for installations with a short period of action.
- Combustion and Ignition