Accession Number : AD0644905

Title :   A STUDY OF SPLITTER EFFECT IN CONICAL DIFFUSERS.

Descriptive Note : Final rept. Jul 63-Aug 66,

Corporate Author : CLEMSON UNIV S C

Personal Author(s) : Yang,Tah-teh

Report Date : AUG 1966

Pagination or Media Count : 3

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.

Descriptors :   (*DIFFUSERS, CONICAL BODIES), BOUNDARY LAYER, RINGS, AIRFOILS, EFFICIENCY, TURBULENCE, INCOMPRESSIBLE FLOW

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE