A Kind of Model-rocket Combustor Test Bed
Abstract
A combustion test bed has been designed in order to study the combustion stability of the rocket engine. In the combustion test bed a cylindrical combustion chamber scheme has been designed and adopted. The diameter, length and nozzle parameters of the combustion chamber have been reasonably selected. The parameters of the combustion chamber can meet the design requirements validated by numerical simulation. Based on the design, the installation and construction of the test bed have been accomplished and it will be used for the research of combustion instability.
Keywords
combustion test bed; cylinder engine; coaxial injector; tangential unstable
DOI
10.12783/dtetr/iceta2016/7085
10.12783/dtetr/iceta2016/7085
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