A STUDY OF SPLITTER EFFECT IN CONICAL DIFFUSERS.

Abstract

The findings of the study were reported at different stages of the progress in various forms with titles as follows: Theory of a thin ring-airfoil in an incompressible inviscid source flow field; The effect of turbulent intensity on the efficiency of conical diffusers; The effect of splitter on turbulence intensity and pressure recovery efficiency in Conical diffusers; Inlet boundary layer effect on the pressure recovery efficiency of conical diffusers with and without a splitter; Splitter effect in conical diffusers part-1 experimental phase incompressible flow; Radius effect of a ring-airfoil on conical diffuser performance; Velocity distribution along the wall of a two-dimensional diffuser with a pair of vanes; Splitter effect in conical diffuser part-2 optimum design of a splitter (ring-airfoil) in a conical diffuser; Splitter effect in conical diffuser part-3 compressibility and scaling effect, experimental-part-4 pressure distribution along a conical diffuser with ring-airfoil, analytical.

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1966
Accession Number
AD0644905

Entities

People

  • Tah-teh Yang

Organizations

  • Clemson University

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Diffusers
  • Efficiency
  • Flow
  • Flow Fields
  • Incompressible Flow
  • Intensity
  • Layers
  • Pressure Distribution
  • Recovery
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.