AEROELASTIC EFFECTS FROM A FLIGHT MECHANICS STANDPOINT.

Abstract

The document is comprised of 27 papers grouped under the following headings: The state-of-the-art; Flight dynamics of a flexible VTOL rotor; Flight dynamics of flexible airplanes (theoretical methods); Experimental methods for flight dynamics of the flexible airplane; Stability and control augmentation devices.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1970
Accession Number
AD0705368

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Dynamics
  • Fixed Wing Aircraft
  • Mechanics

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Control Systems Engineering.
  • Technical Research and Report Writing.