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- W1648167002 abstract "A finite-difference solution to the Navier-Stokes equations combined with a time-varying grid-generation technique was used to compute unsteady transonic flow over an oscillating airfoil. These computations were compared with experimental data (obtained at Ames Research Center) which form part of the AGARD standard configuration for aeroelastic analysis. A variety of approximations to the full Navier-Stokes equations was used to determine the effect of frequency, shock-wave motion, flow separation, and airfoil geometry on unsteady pressures and overall air loads. Good agreement is shown between experiment and theory with the limiting factor being the lack of a reliable turbulence model for high-Reynolds-number, unsteady transonic flows." @default.
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- W1648167002 date "1984-10-01" @default.
- W1648167002 modified "2023-09-23" @default.
- W1648167002 title "Numerical studies of unsteady transonic flow over an oscillating airfoil" @default.
- W1648167002 hasPublicationYear "1984" @default.
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