Patent · US Active

Method for simulating forces applied to a wing in a fluid flow

US11615220B2 · kind B2 · utility

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15Claims
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Key dates

Filing dateJan 4, 2018
Grant dateMar 28, 2023
Priority date
Expiry dateFeb 20, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG06F2119/14
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

A method implemented by a computer for the real-time simulation of a force and/or of a moment applied to a wing in a fluid flow, wherein the body is previously modelled by at least two scalar and vector point sources of a velocity field, the method including at least one of the steps: assessing at least one element selected among a force and a moment, through a linear function dependent on the main velocity vector, V, of the flow; at least one flow rate, referred to as the scalar mass flow rate, As; and at least one flow rate, referred to as the vector mass flow rate, AR, associated with the sources, on at least one point corresponding to one of the sources.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.