Joint US/Russia TU-144 Engine Ground Tests

Abstract

Two engine research experiments were recently completed in Moscow, Russia using an engine from the Tu-144 supersonic transport airplane. This was a joint project between the United States and Russia. Personnel from the NASA Lewis Research Center, General Electric Aircraft Engines, Pratt & Whitney, the Tupolev Design Bureau, and IBP Aircraft LTD worked together as a team to overcome the many technical and cultural challenges. The objective was to obtain large scale inlet data that could be used in the development of a supersonic inlet system for a future High Speed Civil Transport (HSCT). The first experiment studied the impact of typical inlet structures that have trailing edges in close proximity to the inlet/engine interface plane on the flow characteristics at that plane. The inlet structure simulated the subsonic diffuser of a supersonic inlet using a bifurcated splitter design. The centerbody maximum diameter was designed to permit choking and slightly supercritical operation. The second experiment measured the reflective characteristics of the engine face to incoming perturbations of pressure amplitude. The basic test rig from the first experiment was used with a longer spacer equipped with fast actuated doors. All the objectives set forth at the beginning of the project were met.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1997
Accession Number
ADA330104

Entities

People

  • Charles A. Richter
  • Jeffrey S. Balser
  • Mark R. Woike
  • Timothy P. Mccartney
  • Waldo A. Acosta

Organizations

  • Glenn Research Center

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Human Systems

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Boundary Layer
  • Computers
  • Diameters
  • Diffusers
  • Doors
  • Dynamic Pressure
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Subsonic Diffusers
  • Supersonic Inlets
  • Teamwork
  • Trailing Edges
  • Two Dimensional
  • United States

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow