REDUCTION OF CABIN NOISE AND VIBRATION BY INTRINSIC STRUCTURAL TUNING

To control low-frequency interior noise in commercial and general-aviation aircraft, a concept based on intrinsic tuning and damping of the fuselage structural elements has been under development at Boeing for some time. This paper describes the results of some laboratory and field tests that were conducted for evaluation of the concept.

  • Corporate Authors:

    American Institute of Aeronautics and Astronautics

    1290 Avenue of the Americas
    New York, NY  United States  10019
  • Authors:
    • SenGupta, G
  • Publication Date: 1978-6

Media Info

  • Features: References;
  • Pagination: p. 545-546
  • Serial:
    • AIAA Journal
    • Volume: 16
    • Issue Number: 6
    • Publisher: American Institute of Aeronautics and Astronautics

Subject/Index Terms

Filing Info

  • Accession Number: 00188548
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: Feb 27 1979 12:00AM