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- W3175871507 abstract "This work explores the effect of tangential blowing on the vortical structures that develop around a tangent-ogive cylinder configuration at high angle of attack. A lateral force results if blowing is applied asymmetrically. The study is conducted numerically by solving the three-dimensional, compressible-flow Navier-Stokes equations. The computation was done for a Reynolds number of 52,000, Mach number of 0.2, blowing momentum coefficients of 0.0, 0.1, 0.2, and 0.4, and angle of attack of 10, 30, and 45 deg. Only asymmetrical blowing was considered. Surface streamlines, helicity contours and pressure distributions are obtained for each case." @default.
- W3175871507 created "2021-07-05" @default.
- W3175871507 creator A5038517498 @default.
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- W3175871507 date "1991-01-07" @default.
- W3175871507 modified "2023-09-26" @default.
- W3175871507 title "High alpha aerodynamic control by tangential fuselage blowing" @default.
- W3175871507 cites W1988502883 @default.
- W3175871507 cites W2108032536 @default.
- W3175871507 doi "https://doi.org/10.2514/6.1991-620" @default.
- W3175871507 hasPublicationYear "1991" @default.
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