Design minimization of noise in stiffened cylinders due to tonal external excitation

Citation
Ka. Cunefare et al., Design minimization of noise in stiffened cylinders due to tonal external excitation, J AIRCRAFT, 36(3), 1999, pp. 563-570
Citations number
16
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF AIRCRAFT
ISSN journal
00218669 → ACNP
Volume
36
Issue
3
Year of publication
1999
Pages
563 - 570
Database
ISI
SICI code
0021-8669(199905/06)36:3<563:DMONIS>2.0.ZU;2-K
Abstract
A computational design tool was developed to perform a constrained optimiza tion of the acoustic environment within a vibrating cylinder, incorporating finite element and boundary element methods, The tool comprises a UNIX she ll script that coordinates an iterative design optimization process integra ting a number of programs, the key components of which are MSC/NASTRAN for structural analyses, COMET/Acoustics for acoustic analyses, and CONMIN for nonlinear optimization. In addition to the structure and implementation of the tool, this paper presents the results of a number of trials of the tool applied to stiffened and unstiffened cylinders, considering different form ulations of the objective function to be optimized, and for a constant freq uency exterior monopole excitation. Models were constructed to investigate longitudinal vs circumferential variations in design properties as well. Th e results indicate that shell thickness variations tend to dominate interio r acoustic response, as compared with stiffener variations. The results fur ther indicate that longitudinal variation is more effective than circumfere ntial variation. Effective longitudinal design variations include shell thi ckening toward the cylinder midplane or, equally effective, thinning toward the midplane, Effective circumferential designs exhibited periodic variati on around the circumference.