The problem of designing a wing profile with blowing jet on the lower surface at an angle to the contour profile in unlimited stream is set and solved. The iteration process of building solutions is worked out, a series of numerical calculations is made, and conclusions are made.
аэрогидродинамика, крыловой профиль, идеальная несжимаемая жидкость, устройства управления потоком, выдув реактивной струи, aerohydrodynamics, airfoil, ideal incompressible fluid, flow control device, blowing jet
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