Reduction in Flutter Instability of an Elastic Beam with the Rigid Empennage in Supersonic Flow,

Abstract

The possibility of the expansion of the region of dynamic elastic stability of a finned beam streamlined by a supersonic gas flow is investigated. In order to do this a system of automatic control, which consists of the object of control, measuring elements and actuators, is used.

Document Details

Document Type
Technical Report
Publication Date
Nov 18, 1971
Accession Number
AD0736487

Entities

People

  • G. T. Kovbasa
  • I. T. Selezov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Actuators
  • Automatic
  • Flow
  • Gas Flow
  • Instability
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Robotics and Automation.

Technology Areas

  • Hypersonics