NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Study of effects of design details on structural response to acoustic excitationThe normal mode vibration characteristics of one-dimensional and two-dimensional panel arrays were investigated analytically and experimentally. The finite element displacement method was used to formulate the structural models. The structural models include a stiffness and consistent mass matrix for thin-walled open-section beams not previously reported, and a modification of a rectangular plate bending element to include a fundamental interior mode for the element as a generalized coordinate. Provision for adding lumped masses to represent accelerometers is also included. For the one-dimensional panel, the normal mode stress resultants are obtained by integrating the equilibrium equations directly. For the two-dimensional panel arrays, the solution for the stress resultants in the cover sheet was attempted by introducing stress functions dependent upon the displacement field of the plate element. This approach, although incomplete, is a natural extension of the one-dimensional analysis for plate elements. The exerimental program which was used to verify the analysis is described and experimental results are compared with the analysis.
Document ID
19720012271
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rudder, F. F., Jr.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
August 6, 2013
Publication Date
March 1, 1972
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-1959
Report Number: NASA-CR-1959
Accession Number
72N19921
Funding Number(s)
CONTRACT_GRANT: NAS1-9526
PROJECT: RTOP 134-14-06-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available