Transonic 3-D Flow Analysis of Compressor Cascade with Splitter Vanes.

Abstract

Transonic analysis of compressors is performed with and without splitter vanes. This has generally followed five phases of development, proceeding from a single-bladed cascade to splittered cascades, and finally a fully-rotating compressor. The sections in this report describe the basic method (description of geometry, radial equilibrium, and relaxation portions) and comparison data.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1978
Accession Number
ADA057504

Entities

People

  • L. S. Lieber
  • P. R. Dodge

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Blades
  • Compressors
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Equations
  • Flow
  • Fluid Dynamics
  • Geometry
  • Government Procurement
  • Mach Number
  • Pressure Distribution
  • Simulations
  • Static Pressure
  • Three Dimensional
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Molecular Photonics/Laser Physics