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The optimal control of a multi-mass vibration propulsion system in a viscous incompressible fluid propulsion system in a viscous incompressible fluid. The study of the motion is carried out in two stages
Determining the shape of an axisymmetric body in a viscous incompressible flow on the basis of the pressure distribution on the body surfaceDetermining the shape of an axisymmetric body in a viscous incompressible flow on the basis
Determination of optimal parameters of a moving wall on airfoilviscous incompressible fluid
Determining the shape of an axisymmetric body in a viscous incompressible flow on the basis of the pressure distribution on the body surfaceDetermining the shape of an axisymmetric body in a viscous incompressible flow on the basis
The optimal control of a multi-mass vibration propulsion system in a viscous incompressible fluid propulsion system in a viscous incompressible fluid. The study of the motion is carried out in two stages
Theoretical-experimental method of determining the drag coefficient of a harmonically oscillating thin plate harmonically oscillating in a viscous incompressible fluid is proposed. The method is based on measuring
Theoretical-experimental method of determining the drag coefficient of a harmonically oscillating thin plate harmonically oscillating in a viscous incompressible fluid is proposed. The method is based on measuring
Hydrodynamic Damping of Beam Oscillations near a Surface fluid near a plane rigid surface (surface) is investigated. The model of quasi
Determination of optimal parameters of a moving wall on airfoilviscous incompressible fluid
Upper estimates of airfoil aerodynamic characteristics for a viscous incompressible flow in a certain class of airfoils flown by an incompressible flow of viscous fluid at a fixed angle
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