Computational Methods for Feedback Controllers for Aerodynamics Flow Applications

Abstract

This report covers the final results of the STTR: "Computational Methods for Feedback Controllers for Aerodynamics Flow Applications." It is intended to be a comprehensive summary of the project. The goal of the project was to provide a robust, easy to use computational tool for developing feedback controllers for aerodynamic flow applications - i.e. a tool to develop closed loop flow control methods. The two major partners of the STTR were the USAF Academy's Department of Aeronautics, and Cobalt Solutions, LLC (CSLLC).

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Document Details

Document Type
Technical Report
Publication Date
Aug 15, 2007
Accession Number
ADA472029

Entities

People

  • James R. Forsythe
  • Juergen J. Seidel
  • Kelly Cohen
  • Selin Aradag
  • Stefan G. Siegel
  • Thomas E. Mclaughlin
  • William Z. Strang

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programming
  • Computer Programs
  • Control Systems
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Hypervelocity Flow
  • Mathematical Models
  • Neural Networks
  • Standing Waves
  • Three Dimensional
  • Turbulent Mixing
  • Two Dimensional

Readers

  • Computational Fluid Dynamics (CFD)
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Technical Research and Report Writing.