THE PROPERTIES OF A GAS PARTICLE FLOW IN CASCADE.

Abstract

An approximate method is developed for calculating the flow properties of gas-particle mixture flowing over turbine blades in a cascade. Momentum and heat transfer between the gas and particles, as well as compressibility effects were considered. An investigation was made of the effect of particle concentration, mean diameter, particle material density, particle inlet velocity and temperature on the gas particle flow properties on a turbine blade. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1969
Accession Number
AD0697164

Entities

People

  • M.F.M. Hussein
  • Widen Tabakoff

Organizations

  • University of Cincinnati

Tags

DTIC Thesaurus Topics

  • Compressive Properties
  • Diameters
  • Energy Transfer
  • Heat Transfer
  • Materials
  • Momentum
  • Particles
  • Physical Properties
  • Rotor Blades (Turbomachinery)
  • Turbine Blades
  • Turbines
  • Turbomachinery

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerosol Science/Aerosol Physics
  • Combustion science or combustion engineering.