INVESTIGATION OF HIGH GAS TEMPERATURE UTILIZATION FOR ADVANCED TIP TURBINE FANS

Abstract

Studies made of cooling systems for tip-turbine cruise fans are discussed. These studies include a review of planned and predicted core engine exhaust gas conditions; the conceptual design and evaluation of several turbine bucket-carrier cooling systems; sandwich-type double-wall duct constructions; and the definition of advanced material and future test program requirements.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1966
Accession Number
AD0643026

Entities

People

  • M. R. Simonson

Organizations

  • General Electric

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Advanced Materials
  • Air Temperature
  • Army Aviation
  • Boundaries
  • Boundary Layer
  • Ceramic Fibers
  • Fan Blades
  • Flight Speeds
  • Fluid Flow
  • Heat Shields
  • Heat Transfer
  • Internal Pressure
  • Propulsion Systems
  • Static Pressure
  • Thermal Conductivity
  • Turbine Blades

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Systems Analysis and Design