Symmetrical Eigen Forms of the Vibrations of a Supporting Surface and of an Elastic Fuselage,

Abstract

The report discusses a scheme for calculating the frequencies and forms of symmetrical vibrations of two crossed beams, one of which is exposed to bending torsional vibrations (a wing) while the second, only bending ones (a fuselage). The method of collocations is applied by using integral matrixes. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 29, 1973
Accession Number
AD0756285

Entities

People

  • K. M. Shaidukov
  • Z. I. Burman

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Airframes
  • Doppler Effect
  • Frequency
  • Frequency Shift
  • Fuselages
  • Integrals
  • Mathematics
  • Mechanical Structure
  • Vibration

Fields of Study

  • Physics

Readers

  • Structural Dynamics.