High-Fidelity Multidisciplinary Design Using an Integrated Design Environment

Abstract

The main objectives of the research was to further develop the necessary fundamental algorithms to enable high fidelity multi-disciplinary design of complete aircraft configurations. The work was focused on four main areas: (1) Flow solution algorithms for unstructured meshes, (2) Aero-structural plan-form optimization, (3) Multi-fidelity approach to multi-disciplinary design of supersonic aircraft. (4) Algorithms for automatic feedback control of aerodynamic flows.

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Document Details

Document Type
Technical Report
Publication Date
Aug 14, 2007
Accession Number
ADA472441

Entities

People

  • Antony Jameson

Organizations

  • Stanford University

Tags

Communities of Interest

  • Cyber
  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Algorithms
  • Automatic
  • Cargo Aircraft
  • Computational Fluid Dynamics
  • Equations
  • Feedback
  • Fluid Dynamics
  • Geometry
  • Mechanics
  • Optimization
  • Pressure Distribution
  • Reliability
  • Supersonic Aircraft
  • Two Dimensional
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerodynamics/Aeronautics.
  • Computational Fluid Dynamics (CFD)

Technology Areas

  • Hypersonics