Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume II. Addendum. Aerodynamic Redesign

Abstract

This report presents the redesign analysis of the axial compressor program for the advancement of small gas turbine component technology. A two- stage axial compressor was redesigned using test data from the previous two stage tests together with an analysis of a family of high-pressure-ratio compressor rotors. The major changes made to the original design were reduced solidity in both rotors, increased first-stage rotor aspect ratio, and modified first-stage rotor blade profile.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1970
Accession Number
AD0508838

Entities

People

  • Edmund J. Dellert
  • James V. Davis

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Army Aviation
  • Aspect Ratio
  • Boundary Layer
  • Compressor Rotors
  • Compressors
  • Computer Programs
  • Contracts
  • Corporations
  • Diffusion
  • Efficiency
  • Gas Turbines
  • Government Procurement
  • Governments
  • High Pressure
  • Mach Number
  • Turbine Components
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Technical Research and Report Writing.