Aircraft Dynamic Response to Damaged Runways.

Abstract

The three papers included in this Report were presented as the first stage of a study of the potential problems of aircraft dynamic response to damaged and repaired runways, and arrived at the following general conclusions. For small aircraft with relatively simple landing gear, the operation over nominal repairs was dominated by rigid body motions of the aircraft. The prediction of those motions was possible and compared reasonably well with experimental data. For large aircraft or aircraft with large external stores, the prediction of detailed loads in critical areas has met with limited success so far. Since landing gear equations are highly nonlinear, the prediction of aircraft dynamic response has required time-consuming numerical integrations. Also, the behavior of large external stores can be affected by nonlinear effects (such as rigging loads), and both landing gear and external stores nonlinearities are affected by aircraft servicing procedures and by the ambient environment. Papers presented at the 49th Meeting of the Structures and Materials Panel, Porz-Wahn, Germany, October 1979. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1980
Accession Number
ADA085466

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Lift
  • Aircrafts
  • Airframes
  • Center Of Gravity
  • Computer Programs
  • Computer Simulations
  • Computers
  • Dynamic Loads
  • Dynamic Response
  • Landing Gear
  • Mathematical Models
  • Measurement
  • Military Aircraft
  • Nato
  • Nose Wheels
  • Surface Roughness
  • Test Methods

Readers

  • Aerospace Engineering
  • Calculus or Mathematical Analysis
  • Structural Health Monitoring of Composite Structures.