High Fidelity Methods and Physics for UAV Flow Regimes

Abstract

Planned Air Force Unmanned Air Vehicles (UAVs) will be limited by highly nonlinear flow regimes, so an advanced simulation capability has been applied to this class of problems. The proposed paper will document several large-scale computational studies and efforts to validate and to extend the solver capability.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2004
Accession Number
ADP023839

Entities

People

  • Miguel Visbal
  • Raymond Gordnier
  • Reid Melville

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computations
  • Delta Wings
  • Dynamic Response
  • Euler Equations
  • Flow
  • Fluid Flow
  • High Angles
  • Hypervelocity Flow
  • Large Eddy Simulation
  • Physics
  • Unmanned Aerial Vehicles
  • Vibration

Fields of Study

  • Physics

Readers

  • Aerial Unmanned Vehicle Swarm Micro Periodontal Dentistry.
  • Ocean-Atmosphere Mesoscale Modeling, Data Assimilation, and Flux Boundary Layers
  • Operations Research

Technology Areas

  • Autonomy
  • Autonomy - UAVs