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At the University of Liverpool, the Helicopter Multi‐Block (HMB2) CFD code is used for studies of various subsonic and transonic flows. This paper presents the implicit implementation in HMB2 of the AUSM + and AUSM + up, with a fully analytical Jacobian, so that a wider range of Mach numbers can be modelled, including high‐speed flows. A description of the derivation of the analytical Jacobian is...
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