User's Guide - Computer Program - Combustor Reliability Prediction.

Abstract

This document has been written to serve as a guide to the user of the Combustor Reliability Production Program. This program relates burner crack initiation life and louver lip buckling life to the boundary conditions of compressor exit and turbine inlet temperature, expressed as a function of time. A description of the failure mode selection, model development and program sensitivity studies was included in the Final Report (Vol. I) under this contract. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1977
Accession Number
ADA050795

Entities

People

  • B. C. Schlein

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Bending Stress
  • Boundaries
  • Buckling
  • Coatings
  • Coefficients
  • Combustors
  • Computer Programs
  • Computers
  • Engineering
  • Failure Mode And Effect Analysis
  • Instructions
  • Procedures (Computers)
  • Reliability
  • Stresses
  • Turbines

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Computer Science.
  • Software Engineering