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We introduce a new method for estimating the leading edge location of an isolator shock train. This method uses real-time pressure measurements from a small number of transducers to adaptively learn the isolator pressure profile. The deduced profile is subsequently used to estimate the shock train leading edge location in a data-driven manner.

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This page is a summary of: Locating the Isolator Shock-Train Leading Edge with Limited Pressure Information, Journal of Propulsion and Power, June 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38334.
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