INSTRUMENTATION OF THE TRANSONIC TURBINE TEST RIG TO DETERMINE THE PERFORMANCE OF TURBINE INLET GUIDE VANES BY THE APPLICATION OF THE MOMENTUM AND MOMENT OF MOMENTUM EQUATIONS.

Abstract

The primary purpose of the Transonic Turbine Test Rig is to study the effects of axial and radial clearances on turbine performance. Additionally, the installation was designed to permit the determination of stator discharge velocities by the application of the momentum, and moment of momentum equations. Previous attempts to obtain stator discharge velocities by these methods have been unsuccessful. However, during this series of tests, with over 150 hours of useful operating time, the instrumentation and the data acquisition procedures were improved to the extent that the difference between stator discharge velocities obtained from a momentum analysis and those obtained from continuity were reduced to less than three percent. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1967
Accession Number
AD0829411

Entities

People

  • Patrick Michael Commons

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Acquisition
  • Clearances
  • Continuity
  • Data Acquisition
  • Equations
  • Guide Vanes
  • Inlet Guide Vanes
  • Inlets
  • Instrumentation
  • Measuring Instruments
  • Momentum

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Test and Evaluation
  • Plasma Physics.