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47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
The Universal Combustion Device Stability™ (UCDS™) Process is the culmination of more than 40 years of research and provides the means to understand the complex dynamics and processes inside any chemical propulsion system, including rockets, turbojets and scramjets. With UCDS, it is now possible to accurately predict the time history of the pressure oscillation amplitudes during operation. This paper is focused on exploring combustion instability behavior and data analysis. It will start with adoi:10.2514/6.2011-5641 fatcat:h5djhkclqvgnrjun4apgckcwk4