EQUATION OF MOTION OF AN AIRCRAFT WITH A JET ENGINE

Abstract

Equations are given for the motion of an aircraft with a jet engine with variable mass and moments of inertia. The position of the engine and tanks of fuel mixture are considered relative to the center of gravity of the aircraft. For an increase of damping of an aircraft it is expedient to place the jet engine behind the center of gravity at a significant distance.

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Document Details

Document Type
Technical Report
Publication Date
Oct 07, 1963
Accession Number
AD0428550

Entities

People

  • G. M. Trakhtenberg

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Automatic Pilots
  • Center Of Gravity
  • Control Systems
  • Engines
  • Equations
  • Equations Of Motion
  • Exhaust Nozzles
  • Jet Aircraft
  • Jet Engines
  • Moment Of Inertia
  • Relative Motion
  • Rocket Engines
  • Translations
  • Turbojet Engines
  • United States

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Petroleum Engineering