COMMERCIAL SUPERSONIC TRANSPORT PANEL FLUTTER STUDIES

Abstract

The results of analog computer and wind tunnel studies are discussed. The application of the results to design of skin panels for the commercial supersonic transport is discussed. Optimum skin panel design, within the framework of presently existing panel flutter knowledge, is finally discussed. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1964
Accession Number
AD0350412

Entities

People

  • C. H. Hodson
  • J. E. Stocker

Tags

DTIC Thesaurus Topics

  • Analog Computers
  • Computers
  • Computing Devices
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Structural Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow