3-D Stress Analysis of a turbine Blade

Abstract

This report presents a demonstration of the usefulness of the ATLAS system in performing three-dimensional elastic stress analysis of a turbine blade. Modeling details for a shrouded uncooled turbine blade are outlined and program execution and data management techniques are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1977
Accession Number
ADA039176

Entities

People

  • C. M. Lewis
  • F. Yen
  • R. A. Samuel

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Army Aviation
  • Centrifugal Force
  • Commercial Aircraft
  • Computers
  • Data Management
  • Geometry
  • Helicopters
  • Materials
  • Mechanics
  • Three Dimensional
  • Transport Aircraft
  • Turbine Blades
  • Turbines
  • Two Dimensional
  • United States

Readers

  • Aerodynamics.
  • Business Analytics
  • Structural Health Monitoring of Composite Structures.