Computational and Physical Aspects of UAV Vortical Flows

Abstract

Briefing charts from presentation on the computational and physical aspects of UAV(unmanned air vehicle) vortical flows.

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Document Details

Document Type
Technical Report
Publication Date
Jul 26, 2004
Accession Number
ADA428824

Entities

People

  • Miguel R. Visbal

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Boundary Layer
  • Delta Wings
  • Flow
  • Flow Fields
  • Information Operations
  • Layers
  • Military Research
  • Secondary Flow
  • Trailing Edges
  • Turbulent Mixing
  • Unmanned Aerial Vehicles
  • Vehicles

Technology Areas

  • Autonomy