A Simple Analytical Theory for Interpreting Measured Total Pressure in Multiphase Flows

Author:

Guha Abhijit1

Affiliation:

1. Whittle Laboratory, University of Cambridge, Madingley Road, Cambridge CB3 0DY, U.K.

Abstract

This paper presents a simple, analytical theory for determining total pressure in multiphase flows, a subject of theoretical interest as well as of practical importance. It is shown here that the nonequilibrium processes occurring in the vicinity of a measuring device have a significant influence on the magnitude of flow velocity inferred from Pitot measurements. The present theory predicts that, depending on the size of the particles or droplets, the total pressure varies monotonically between the two limiting values: the frozen total pressure (when there is no interphase mass, momentum, and energy transfer in the decelerating flow toward the stagnation point) and the equilibrium total pressure (when the dispersed phase, either liquid droplets, or solid particles, is always at inertial and thermodynamic equilibrium with the continuous vapour phase). The presented analytical theory is a relation between nondimensional total pressure and Stokes number, representing particle size or inertia, and specifies the total pressure under different nonequilibrium conditions. One simple equation applies to diverse multiphase mixtures, solid particle laden gas as well as vapour-droplet mixtures, and at a wide range of flow conditions, both subsonic and supersonic. The associated issue of interpreting total temperature, and the relation between measured total pressure and entropy production in multiphase flows have been discussed at length by Guha (1998).

Publisher

ASME International

Subject

Mechanical Engineering

Reference10 articles.

1. Crane R. I. , and MooreM. J., 1972, “Interpretation of Pitot Pressure in Compressible Two-Phase Flow,” Journal of Mechanical Engineering Science, Vol. 14, No. 2, pp. 128–133.

2. Dussourd J. L. , and ShapiroA. H., 1958, “A Deceleration Probe for Measuring Stagnation Pressure and Velocity of a Particle-Laden Gas Stream,” Jet Propulsion, Vol. 28, pp. 24–34.

3. Guha, A., and Young, J. B., 1991, “Time-Marching Prediction of Unsteady Condensation Phenomena Due to Supercritical Heat Addition,” Proc. Conf. Turbomachinery: Latest Developments in a Changing Scene, London. IMechE, pp. 167–177.

4. Guha A. , 1992, “Structure of Partly Dispersed Normal Shock Waves in Vapour-Droplet Flows,” Physics Fluids, Vol. 4, No. 7, pp. 1566–1578.

5. Guha, A., 1995, “Two-Phase Flows with Phase Transition,” VKI Lecture Series, 1995-06 (ISSN0377-8312), pp. 1–110, von Karman Institute for Fluid Dynamics.

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