Application of System Identification Techniques to Turbine Engine Post-Stall Test and Evaluation. Volume 1

Abstract

Application of System Identification Techniques to Turbine Engine Post-Stall Test and Evaluation was an Air Force funded study to investigate and apply system identification techniques to post-stall engine models in a manner which allowed AEDC personnel to become proficient in the use of these techniques. The final technical report for the second phase of this study is divided into two volumes. This, the first volume, describes the estimation of post-stall characteristics of a 10-stage compressor rig model, using rig test data. Volume II describes the application of parameter estimation theory to gas turbine engines and the use of the SCIDNT estimation code used in this effort.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1990
Accession Number
ADA239181

Entities

People

  • Robert P. Anex

Tags

Communities of Interest

  • Energy and Power Technologies
  • Human Systems
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Air Force
  • Compression
  • Compressors
  • Computational Fluid Dynamics
  • Computer Programs
  • Data Analysis
  • Data Sets
  • Digital Data
  • Engineering
  • Gas Turbines
  • Measurement
  • Pressure Measurement
  • Research Facilities
  • Technology Transfer
  • Test And Evaluation
  • Turbines
  • United States

Fields of Study

  • Engineering

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerospace Engineering
  • Instructional Design and Training Evaluation.