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F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
F16D33/00—Rotary fluid couplings or clutches of the hydrokinetic type
F16D33/02—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the flow of the liquid in the working circuit, while maintaining a completely filled working circuit
F16D33/04—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the flow of the liquid in the working circuit, while maintaining a completely filled working circuit by altering the position of blades
Cryptosteady-flow energy separation(Cryptosteady flow energy separation mechanisms, considering bearing friction and rotor torque effects and rotor nozzle proportion equations)
Performance of the cryptosteady flow energy separator(Development of performance equations for cryptosteady-flow energy separator over widest range of operating conditions for turbojet engines)
Turbulent boundary layer studies on a waisted body of revolution in subsonic and supersonic flow(Experimental and theoretical turbulent boundary layer interrelations in supersonic flow with friction coefficients)
Considerations on the instantaneous potential of velocities in a viscous fluid flow(Viscous fluid flow velocities instantaneous potential based on continuous medium, energy conservation and classic kinetic matter theories)
Development of a boundary layer in the inlet section of a tube in the case of injection(Fluid flow turbulent boundary layer development in channel inlet under injection, obtaining friction coefficient and dynamic characteristics at subsonic velocities)
The establishment of a relationship between the intensity value and the dissipation of energy of turbulence(Flow velocity fluctuation intensity relationship to turbulent energy dissipation based on Kolmogoroff similarity hypothesis)
Unsteady hypersonic wake behind blunt bodies, showing relation between transition and vortex formation and the variation of strouhal number with reynolds number
On the'reflection' of the Mach cones at the subsonic leading edges of a thin wing in supersonic flow(Mach cones reflection at thin wing subsonic leading edges in supersonic flow, considering axial disturbance velocity and pressure distributions)
Hydrodynamic forces on an oscillating circular cylinder with a pair of trailing vortices developed behind the cylinder(Hydrodynamic forces on oscillating cylinder with trailing vortices)[Ph. D. Thesis]
Pressure drop and entropy production in a viscous adiabatic pipe flow at low flow velocity(Pressure drop relation to entropy production in viscous low velocity adiabatic pipe flow, showing analogy with Oswatitsch theorem)
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