3rd AIAA/CEAS Aeroacoustics Conference 1997
DOI: 10.2514/6.1997-1620
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Stiffener shape design to minimize interior noise

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Cited by 3 publications
(3 citation statements)
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“…For the acoustic characteristics to be influenced, we can name the sound power, sound pressure level, directivity patterns or other measures. Approaches to formulate an objective function to judge the desired properties can be categorized into three different groups, the first one being the sound pressure level at one or more specified points, primarily utilized for closed domains [28,64,86]. For general-purpose noise control in open domains, the emitted sound power accounted for the objective function in a number of papers [10,16,50,57,58].…”
Section: Acoustic and Structural-acoustic Optimizationmentioning
confidence: 99%
“…For the acoustic characteristics to be influenced, we can name the sound power, sound pressure level, directivity patterns or other measures. Approaches to formulate an objective function to judge the desired properties can be categorized into three different groups, the first one being the sound pressure level at one or more specified points, primarily utilized for closed domains [28,64,86]. For general-purpose noise control in open domains, the emitted sound power accounted for the objective function in a number of papers [10,16,50,57,58].…”
Section: Acoustic and Structural-acoustic Optimizationmentioning
confidence: 99%
“…One idea is to optimize the shape or the material properties of the fuselage so that characteristic frequencies of the interior space do not match the tones in the propeller noise spectrum. 22 Another idea is to optimize the sound produced by an array of loudspeakers so that the noise due to the propeller is canceled by the "anti-noise" produced by the speakers. 23 A third idea is to optimize the inputs to inertial actuators attached to the airframe so that the vibration of the fuselage is reduced.…”
Section: Noise Controlmentioning
confidence: 99%
“…An interesting study of optimally distributed damping material on a circular plate has been provided by Wodtke and Lamancusa. 56 More realistic applications were discussed by Cunefare and Engelstad et al [10][11][12] Their example, a cylinder clamped at both ends and acoustically excited by a monopole source from outside appears roughly similar to an aircraft fuselage. However, investigation of shell thickness optimization as well as optimal positioning of stringers and frames for stiffening look reasonable to conclude for more complex aircraft constructions.…”
Section: Introductionmentioning
confidence: 97%