Platform Design & Structures Technologies

Abstract

Enables new rotorcraft configurations by evaluating critical advanced aviation technologies using design and analysis methods with greater modeling fidelity with an ultimate goal of reducing the timelines associated with overall design of new aircraft. Introduces high fidelity methodology for improved performance and design predictions earlier in the development and acquisition process. Use physics of failure modeling and coupled discipline analysis to drastically improve component and system reliability. Work is coordinated with Aviation Component Failure Modeling efforts in PE 0602211, Project 47B at Army Research Laboratory (ARL).

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2015
Source ID
794bda6c38b452f87ef2cb0f0a9592df

Tags

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Military Science and Technology Research and Modernization.
  • Software Engineering.

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