THE USE OF CROSS CORRELATION IN STUDYING THE RESPONSE OF LIGHTLY DAMPED STRUCTURES TO NOISE.

Abstract

It is the purpose of this note to study the application of cross - correlation techniques to determine the overall frequency response to random forces of a typical aerospace vehicle structure. The effect of truncation of the cross correlation function in the estimated cross spectrum is discussed with reference to a single degree of freedom system excited by white noise. Application to multi degree of freedom systems is discussed and an ullustration is given of the use of the technique in the analysis of panel vibration in a typical rear fuselage excited by jet noise. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1966
Accession Number
AD0484558

Entities

People

  • B. L. Clarkson

Organizations

  • University of Southampton

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerospace Craft
  • Airframes
  • Correlation Techniques
  • Cross Correlation
  • Data Science
  • Frequency
  • Frequency Response
  • Frequency Shift
  • Fuselages
  • Information Science
  • Mathematics
  • Noise
  • Spectra
  • Structural Components
  • Truncation
  • White Noise

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Aerodynamics/Aeronautics.
  • Control Systems Engineering.

Technology Areas

  • Space