Static Aeroelasticity in Combat Aircraft.

Abstract

This publication contains three papers presented to the Aeroelasticity Sub-Committee of the AGARD Structures and Materials Panel at its 60th Meeting. The papers show that static aeroelasticity is increasingly being considered as a primary design parameter, affecting as it does structural optimisation, vehicle aerodynamic stability control effectiveness and overall performance.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1986
Accession Number
ADA167595

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Composite Materials
  • Control Systems
  • Fighter Aircraft
  • Fluid Dynamics
  • Fuselages
  • Geometry
  • High Lift Devices
  • Mach Number
  • Spars
  • Stabilization Systems
  • Swept Wings
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerodynamics/Aeronautics.
  • Systems Analysis and Design