On the flow of gases at high speeds

Author:

Abstract

In a paper on the discharge of gases under high pressures* the late Lord Rayleigh called attention to the deficiencies in the present state of knowledge of the characteristics of the flow of a gas, from a vessel in which it is compressed, through an orifice into the atmosphere or into a receiver at a lower pressure, and suggested that further study was desirable in the direction of investigating the accuracy of the common assumptions of the adiabatic character of the flow and its dependence on the pressure in the receiver. Assuming adiabatic flow the values of the velocity of the jet and the rate of discharge are given by the well-known relations- u 2 /2 = γ/γ-1. p 0/ρ0{1-( p / p 0)γ-1/γ}, w = g A√ 2γ/γ-1. p 0ρ0( p / p 0)2/γ {1-( p / p 0)γ-1/γ}, where u is the speed, p and A the pressure and area of the jet, and w the rate of discharge, the suffix 0 referring to the conditions inside the discharging vessel where u = 0.

Publisher

The Royal Society

Subject

General Medicine

Cited by 20 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. THE CRITICAL ORIFICE REVISITED - A NOVEL LOW-PRESSURE DROP CRITICAL ORIFICE;AM IND HYG ASSOC J;1984

2. Flow in Nozzles and Jets;Applied Mathematical Sciences;1976

3. Contraction coefficients for compressible flow through axisymmetric orifices;International Journal of Mechanical Sciences;1970-05

4. A Non-Equilibrium Low Vapor Pressure Heat of Vaporization Calorimeter. Part I. Vapor Pressure Range 200-10^-3 mm Hg.;Acta Chemica Scandinavica;1968

5. Paper 7: An Investigation of Steady Compressible Flow through Thick Orifices;Proceedings of the Institution of Mechanical Engineers, Conference Proceedings;1965-06

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