The phrase "as a nozzle" is correct and usable in written English.
It can be used in contexts related to mechanics, engineering, or fluid dynamics, where a nozzle is a device designed to control the direction or characteristics of fluid flow.
Example: "The design of the spray system incorporates a unique feature that allows it to function effectively as a nozzle."
Alternatives: "in the role of a nozzle" or "serving as a nozzle."
As a nozzle man, he probably could put out the whole building if there was a fire.
The function of the diaphragm is to regulate the pressure of air, while the larynx, as a nozzle in a water spray, determines the nature of the flow.
Thus NACA airfoil shape [27] was suggested to be deployed in the channels as a nozzle, since it incorporated these two important parameters.
Noise predictions are presented for both a smooth convergent-divergent nozzle as well as a nozzle representative of a military aircraft engine.
In this case, two different negative effects occur: the cumulative working surface of parallel slides stack is less than the rolled stack surface; moreover the plastic frame behaves as a nozzle that can produce little variations in the resonance frequency of the tube (Fig. 6).
In this case, two different negative effects occur: the cumulative working surface of parallel slide stack is less than the rolled stack surface; moreover, the plastic frame behaves as a nozzle that can produce little variations in the resonance frequency of the tube (Figure 6).
HWB treatment at 55°C was applied on the packing line, as a spray (nozzle pressure of 2 atm) above brushes revolving at 60 g, a rate of 100 120 L min-1 and at a nozzle pressure of 2 atm [ 2].
The superiority of the proposed approach over mesh refinement algorithms which employ standard unweighted (type II) error indicators, which do not require the solution of an auxiliary problem, are illustrated by a series of numerical experiments; here, we consider transonic flow through a nozzle, as well as subsonic and supersonic flows around different airfoil geometries.
The tip diameter of the rotor was 80 mm and the nozzle was designed as a supersonic nozzle to increase the turbine output power.
It also includes a 0.8mm nozzle diameter — as well as a 0.4mm nozzle — for speedier (but less fine) print-outs.
In others the propellant is accelerated without a nozzle (as in the ion and Hall thrusters) by electromagnetic means, in which case at least part of the fluid must be electrically charged first.
