Flutter Analysis of an All-Movable Horizontal Tail with Geared Elevator on a Supersonic Transport

Abstract

This document presents symmetric flutter analyses conducted on the all-movable horizontal tail of the Boeing-designed SST. Interaction effects on flutter speed that are produced by the wing, fuselage, control systems and elevator gear ratio are included. Failure conditions of the horizontal-tail actuators are covered.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1974
Accession Number
ADB000285

Entities

People

  • Jerry L. Stelma

Organizations

  • Boeing

Tags

Communities of Interest

  • Cyber

DTIC Thesaurus Topics

  • Actuators
  • Aerodynamic Forces
  • Aircrafts
  • Airplanes
  • Boundaries
  • Commercial Aircraft
  • Control Systems
  • Equations
  • Equations Of Motion
  • Frequency
  • Fuselages
  • Horizontal Stabilizers
  • Hydraulic Actuators
  • Mach Number
  • Supersonic Transport Aircraft
  • Surfaces
  • Transfer Functions

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Software Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow