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Gallital Iberica S A
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Gallital Iberica S A
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Structures Of Non-Positive Displacement Pumps
(AREA)
Hydraulic Turbines
(AREA)
Abstract
Dispositivo lavaparabrisas, caracterizado por el hecho de constar de un elemento deformable impulsor y succionador empalmado mediante conductos apropiados a una válvula de retorno en T una de cuyas bocas se une a un depósito de líquido y la otra a la boquilla de salida del líquido con poniendo, con sus tres bocas, dos salidas y dos entradas según la actuación de sus válvulas e impulsiones y succiones produciendo, en determinados momentos la salida en chorro del líquido a través de las boquillas en rótula direccional y con modificación del coeficiente aerodinámico merced a escabas previstas en la cara activa de la propia boquilla, con lo que el vector de la componente de salida producido por la velocidad será anulado y mantenido en el valor primitivo.
Wind tunnel measurements of the effect of a jet on the time average and unsteady pressures on the base of a bluff afterbody(Time average and unsteady pressures on base of blunt afterbody, containing single jet, measured in subsonic and transonic air streams)
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)
Dynamic simulation of supersonic inlet and engine(Transient response in dynamic simulation of supersonic inlet and engine combination used to determine control requirements of sst propulsion system)
Effect of flow vorticity on friction and heat transfer as applied to a supersonic jet impinging on an obstacle(Vorticity effects on drag friction and heat transfer near stagnation point of supersonic jet impinging on obstacle)
Effect of turbulence on heat transfer in a supersonic jet with plane obstacle(Turbulent flow effect on heat transfer in supersonic jet with plane infinite obstacle perpendicular to jet axis)
Initial'' supersonic flow and supersonic waves at the outlet of a plane nozzle(Initial supersonic flow and supersonic waves at outlet of plane nozzle by reducing rheological method to two related problems in gas dynamics)
Pressure acting on the oscillating surface of an airfoil in nonlinear supersonic potential flow(Pressure distribution acting on oscillating airfoil surface in nonlinear supersonic potential flow, considering steady perturbed stream effect on unsteady flow)
Relevance of the pressure jump/or instability/ and a strong southerly flow with a low-level jet and associated inversion as a situation for low- level turbulence, even in clear air