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- W2326348510 abstract "An interacting boundary layer procedure using the Veldman quasi-simultaneous method h a s been developed for an unsteady compressible boundary layer coupled with the high frequency transonic small disturbance equation. The matching condition is based on the asymptotic technique of Davis, Werle and Van Dyke. The method has been verified for a variety of oscillating airfoil cases. Comparison with experiment is made, and oscillating airfoil cases computed with light shock induced stall. A comparison of two algebraic turbulence models shows that there is an extreme sensitivity of shock-induced flow to slight differences in turbulence modeling. Finally a self-induced oscillatory solution of the 18% circular arc airfoil shows a favorable comparison with experiment." @default.
- W2326348510 created "2016-06-24" @default.
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- W2326348510 date "1994-06-20" @default.
- W2326348510 modified "2023-09-25" @default.
- W2326348510 title "An unsteady interacting boundary layer method for oscillating airfoils experiencing light shock-induced stall" @default.
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- W2326348510 doi "https://doi.org/10.2514/6.1994-2341" @default.
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