Air Vehicle Structures and Dynamics Technology

Abstract

This Project establishes validated modeling tools needed to develop aeroelastically stable rotor technologies to enable high speed flight and longer flight envelopes in Future Vertical Lift (FVL) platforms. Efforts in this Project are also applicable to the family of Future Vertical Lift manned and unmanned platforms. Work in this Project is fully coordinated with PE 0603465A (Future Vertical Lift Advanced Technology Development). The cited work is consistent with the Under Secretary of Defense for Research and Engineering Science and Technology focus areas and the Army Modernization Strategy.

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Document Details

Document Type
Project
Publication Date
Oct 01, 2020
Source ID
AL5_0602148A_2_2040_PB_2020

Tags

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Military Science and Technology Research and Modernization.

Technology Areas

  • Autonomy
  • Autonomy - Autonomous System Control

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