Experimental Study of the Effect of Subsonic Exhaust Gas Diffusers on the Test Cell Wall and TF39 Cold-Flow Model Engine Exhaust Nozzle Plug and Core Engine Cowl Surface Pressures

Abstract

An experimental investigation was conducted to determine the effects of exhaust gas collectors/subsonic diffusers on engine and test cell surface pressures during tests of high-bypass-ratio front-fan engines in ground test facilities. A one-tenth scale model of a TF39 turbofan engine installed in a one-tenth scale model of Propulsion Development Test Cell (J-1) was employed. Engine cowl and plug surface pressure data were recorded during model engine operation with cold air at five simulated power settings without exhaust collector, with exhaust collector, with exhaust collector equipped with a conventional subsonic diffuser, and with exhaust collector equipped with a segmented subsonic diffuser which separately diffused the fan and core engine exhaust jets.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1973
Accession Number
AD0759177

Entities

People

  • Delbert Taylor
  • Frank T. Lee
  • Marvin Simmons

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accumulators
  • Air Force
  • Air Supplies
  • Cellular Structures
  • Diffusers
  • Engines
  • Exhaust Gases
  • Flow Fields
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Scale Models
  • Stagnation Pressure
  • Static Pressure
  • Subsonic Diffusers
  • Test Facilities
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.