The Effect of Dynamic Ground Loads on an Aircraft Wing,

Abstract

The author investigates the reaction of an aircraft wing in its bending by impact and periodic loads of landing gears in relationship to weight parameters of the wing, damping and frequency of periodic load. The investigation was conducted on an electric aircraft wing simulator. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 05, 1972
Accession Number
AD0747381

Entities

People

  • V. S. Mukho

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Wings
  • Aircrafts
  • Airframes
  • Frequency
  • Landing Gear
  • Simulators

Readers

  • Aerodynamics/Aeronautics.
  • Approximation Theory.
  • Electrical Engineering