Evolution of the Turbulence Wakes Behind Inlet Guide Vanes,

Abstract

Experimental results obtained from turbine exit cascades were studied to determine their applicability as compressor inlet guide vanes. The experimental investigations included wind tunnel studies (at M = 0.12) in which the inlet turbulence intensity was determined. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 18, 1968
Accession Number
AD0852524

Entities

People

  • J. Elsner

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Compressors
  • Control Surfaces
  • Control Systems
  • Guide Vanes
  • Inlet Guide Vanes
  • Inlets
  • Intensity
  • Openings
  • Personal Information Managers
  • Surfaces
  • Turbulence
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.