Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine

Leslie W. Lassiter, Robert W. Hess
naca-tn-4076
Sep 1957


Flat 2024-T3 aluminum panels measuring 11 inches by 13 inches were tested in the near noise fields of a 4-inch air jet and turbojet engine. The stresses which were developed in the panels are compared with those calculated by generalized harmonic analysis. The calculated and measured stresses were found to be in good agreement.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-tn-4076.pdf