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- W2008010968 abstract "An integral equation of the transonic small-disturbance differential equation is extended to second order for supersonic flows around three-dimensional thin wings, allowing bow as well as embedded shock waves. An explicit solution of the second-order small-disturbance equations satisfying the second-order boundary conditions of a wing is obtained. The particular solution is expressed as the differentiation of a volume integral with specifically chosen boundaries, and the complementary solution satisfies the linearized velocity potential equation with appropriate boundary conditions. A numerical procedure based on this solution for three-dimensional wing calculations is proposed. The flows about a delta wing with a wedge cross section and a supersonic leading edge at zero attack angle are calculated by the numerical methods." @default.
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- W2008010968 date "1996-12-01" @default.
- W2008010968 modified "2023-10-16" @default.
- W2008010968 title "Second-order small-disturbance solution for wing at supersonic speeds" @default.
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- W2008010968 doi "https://doi.org/10.2514/3.13439" @default.
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