Liquid rocket thrust chamber test run inner wall temperature calculation method and calculation equipment
A technology of liquid rockets and calculation methods, applied in design optimization/simulation, special data processing applications, etc., can solve the problems of incomparability and the inability to obtain the wall temperature of the thrust chamber, and achieve the effect of improving the probability of success and facilitating structural parameters.
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[0033] The present disclosure will be further described in detail below with reference to the drawings and embodiments. It can be understood that the specific implementation manners described here are only used to explain relevant content, rather than to limit the present disclosure. It should also be noted that, for ease of description, only parts related to the present disclosure are shown in the drawings.
[0034] It should be noted that, in the case of no conflict, the implementation modes and the features in the implementation modes in the present disclosure can be combined with each other. The present disclosure will be described in detail below with reference to the drawings and embodiments.
[0035] see figure 2 A simplified schematic of the thrust chamber heat transfer structure shown, and image 3 A schematic diagram of the enlarged structure is shown. The side wall of the thrust chamber extends in a cylindrical shape around the axis of the thrust chamber, and g...
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