Accession Number : ADA130296

Title :   Effects of Interstage Diffuser Flow Distortion on the Performance of a 15.41-Centimeter Tip Diameter Axial Power Turbine.

Descriptive Note : Technical memo.,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CENTER

Personal Author(s) : McLallin,Kerry L ; Kofskey,Milton G ; Civinskas,Kestutis C

PDF Url : ADA130296

Report Date : Jan 1983

Pagination or Media Count : 24

Descriptors :   *Axial flow turbines, *Diffusers, *Ducts, *Performance(Engineering), Inlets, Boundary layer flow, Turbine stators, Turbine blades, Measurement, Rotor blades

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE