STRUCTURAL SCALE LIFE PREDICTION OF AERO STRUCTURES EXPERIENCING COMBINED EXTREME ENVIRONMENTS

Abstract

Reusable high-speed air platforms are critical to the global reach and superiority of tomorrows USAF. These platforms experience long-duration, combined and intense, thermo-mechanical-acoustic loads over significant portions of their structure. Designing and fielding these platforms requires the capability to probabilistically assess the structural life under complex loading environments. Todays state of the art methods cannot address structural reliability under combined environment conditions due to inadequate understanding of the interactions between the various applicable material failure mechanisms and the continuously-evolving material/structural states. Lack of the necessary knowledge has resulted in significant repair and replacement costs for existing USAF platforms like the B-2 where zones of the aircraft are required to operate under combined, thermo-acoustic-mechanical loads. Current practices for margin prediction are rooted in analysts past experience, a heavy reliance on testing, and limited choices to tailor material attributes.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2017
Accession Number
AD1036190

Entities

People

  • Ravinder C. Chona
  • Thomas Iii G. Eason

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Algorithms
  • Engineering
  • Environment
  • Extreme Environments
  • Failure Mode And Effect Analysis
  • Fatigue Life
  • Governments
  • Grain Boundaries
  • J Integrals
  • Materials
  • Mechanics
  • Military Research
  • Platforms
  • Reliability

Fields of Study

  • Engineering

Readers

  • Structural Health Monitoring of Composite Structures.
  • Systems Analysis and Design
  • Unmanned Aerial System (UAS) Autonomous Capabilities and Mission Reconnaissance.