Temperature test of motor combustion gas flow field with thermographic instrument
Journal of Solid Rocket Technology(2003)
Abstract
Radiant temperature of solid rocket motor combustion gas flow field was tested and measured by means of infrared thermographic instrument on the basis of the experiment, and the test results were analyzed and treated through data calibration of high temperature wind tunnel. The method for setting up the radiant coefficient is put forward to solve the infrared radiation temperature measurement problem for motor combustion gas flow field.
MoreTranslated text
Key words
thermographic instrument,temperature,combustion,flow field
AI Read Science
Must-Reading Tree
Example
![](https://originalfileserver.aminer.cn/sys/aminer/pubs/mrt_preview.jpeg)
Generate MRT to find the research sequence of this paper
Chat Paper
Summary is being generated by the instructions you defined