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Showing 1 to 4 of 4 for “"Shock sensor"”.

  1. Use of a triboelectric generator for a tunable wideband energy harvester and a threshold shock sensor

    … outputs. A proof of concept of a threshold shock sensor is proposed that incorporates bi-stability along with the triboelectric effect. A clamped-clamped buckled beam will switch stable states when a threshold shock amplitude is experienced and a voltage peak will occur during this switching …

    binghamton Repository record for Use of a triboelectric generator for a tunable wideband energy harvester and a threshold shock sensor (opens in a new tab)

  2. On the Application of an Output-based Adaptive, Higher-order Finite Element Method to Sonic Boom Propagation

    … artificial viscosity is incorporated via a shock sensor PDE approach to handle shock presence, with necessary corrections applied to the DWR error estimate. The VMSD-BR2 method is applied then to a real-world scenario solving the augmented Burgers equation, which models the propagation of …

    mit Repository record for On the Application of an Output-based Adaptive, Higher-order Finite Element Method to Sonic Boom Propagation (opens in a new tab)

  3. Shock capturing with PDE-based artificial viscosity for an adaptive, higher-order discontinuous Galerkin finite element method

    … greater than the speed of sound, an appropriate shock capturing for higher-order, adaptive methods is necessary. Artificial viscosity can be combined with a higher-order discontinuous Galerkin finite element discretization to resolve a shock layer within a single cell. However, when a nonsmooth …

    mit Repository record for Shock capturing with PDE-based artificial viscosity for an adaptive, higher-order discontinuous Galerkin finite element method (opens in a new tab)

  4. Numerical Modelling of Shock Wave Boundary Layer Interactions in Aero-engine Intakes at Incidence

    … flow to supersonic speeds, terminating with a shock wave. This produces undesirable shock wave boundary layer interactions (SWBLIs). Reynolds-Averaged Navier Stokes (RANS) turbulence models have been shown to be insensitive to the effects of boundary layer relaminarisation present in these …

    cambridge Repository record for Numerical Modelling of Shock Wave Boundary Layer Interactions in Aero-engine Intakes at Incidence (opens in a new tab)