The Operation of a Two-Chamber Pneudraulic Shock Absorber

Abstract

For the most common types of two chamber, pneumohydraulic shock absorbers for S type landing gear, the author presents the functions permitting the shock absorber's initial charging, motion, and force parameters, which arise during the static and dynamic compression of the landing gear by different methods, to be defined. The shock absorber's operational equations, allow the author to create a generalized program for computer solution of the system of dynamic equations of the motion of a landing gear with different types of one chamber and two chamber shock absorbers.

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Document Details

Document Type
Technical Report
Publication Date
Jan 04, 1973
Accession Number
AD0754609

Entities

People

  • N. A. Melik-zade

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Absorption
  • Abstracts
  • Air
  • Air Force
  • Air Pressure
  • Air Resistance
  • Aircrafts
  • Compressed Air
  • Differential Equations
  • Equations
  • Equations Of Motion
  • Fluid Flow
  • Fluids
  • Foreign Technology
  • Landing Gear
  • Security
  • Shock Absorbers

Readers

  • Aerospace Engineering
  • Electrical Engineering
  • Explosive Engineering.