Airplane Stability for Flight with Constant Angular Velocity around the Longitudinal Axis,

Abstract

The paper considers the effects of longitudinal acceleration and magnus forces and moments on stability of aircraft having single plane of symmetry and gives expressions allowing estimation of cases when such effects should be taken into account. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 29, 1971
Accession Number
AD0738231

Entities

People

  • Milorad Pastrakuljic

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Fixed Wing Aircraft
  • Motion
  • Physical Properties
  • Symmetry
  • Vehicles
  • Yugoslavia

Readers

  • Control Systems Engineering.