EFFECTS OF AEROELASTICITY ON THE STABILITY AND CONTROL CHARACTERISTICS OF AIRPLANES,

Abstract

The effects of aeroelasticity on stability and control are discussed under the two general categories of longitudinal and lateral motion. In each case the effects of wing, fuselage, and tail flexibility on stability of motion and effectiveness of control are considered for various flight conditions including dynamic pressure and Mach number. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1961
Accession Number
AD0446167

Entities

People

  • F. V. Bennett
  • H. L. Runyan
  • K. G. Pratt

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Aeroelasticity
  • Aircrafts
  • Airframes
  • Airplanes
  • Dynamic Pressure
  • Fuselages
  • Mach Number
  • Mechanical Properties
  • Mechanics
  • Physical Properties
  • Resilience
  • Training

Fields of Study

  • Mathematics
  • Physics

Readers

  • Aerospace Engineering
  • Plasma Physics / Magnetohydrodynamics