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- W2032928305 abstract "In the present investigation, the 'thin layer' Navier-Stokes equations are used to compute the flow about a delta wing and a strake-delta wing configuration. Both configurations possess blunt noses and rounded leading edges. The computational grid about these configurations is generated using a newly developed three-dimensional grid-generation code which solves a set of Poisson equations with spherical coordinate variables using an alternating direction implicit (ADI) scheme. Computational results are obtained for an isolated wing with 60 deg sweep and a strake-wing configuration with 80-60 deg sweep. Computations for angles of attack in the range from 6 to 30 deg are presented. Attention is given to the effect of the angle of attack, the Mach number, and the Reynolds number. Theoretical results are compared with experimental data." @default.
- W2032928305 created "2016-06-24" @default.
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- W2032928305 date "1983-07-13" @default.
- W2032928305 modified "2023-09-27" @default.
- W2032928305 title "Numerical simulation of the leading-edge separation vortex for a wing and strake-wing configuration" @default.
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- W2032928305 doi "https://doi.org/10.2514/6.1983-1908" @default.
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