Application of Approximate Inertial Manifolds and Multiresolution Techniques to Parallel Computations of Sensititives and Design

Abstract

The objective of this work is to develop methodologies for the efficient computation of aerodynamic sensitivities using state-of-the-art CFD techniques for use in aerodynamic shape optimization and fluids-structure interaction analysis including: analysis of multiresolution schemes to compute sensitivities, analysis of parallel implementation issues in sensitivity computations, modification of a production CFD code for parallel multiresolution computation of sensitivities, integration of sensitivities into airframe optimization.

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Document Details

Document Type
Technical Report
Publication Date
Mar 14, 1998
Accession Number
ADA381583

Entities

People

  • Gail Berkooz

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Wings
  • Aircrafts
  • Airframes
  • Computational Fluid Dynamics
  • Computations
  • Electronic Mail
  • Flexible Structures
  • Flow
  • Fluid Dynamics
  • Geometry
  • Mechanical Engineering
  • Mechanical Structure
  • Optimization
  • Parallel Computing
  • Sensitivity
  • Three Dimensional

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation
  • Control Systems Engineering.