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Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:59:56Z
date available2017-09-04T17:59:56Z
date copyright01/01/1955
date issued1955
identifier otherFVNUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/183044
description abstractSubsonic and supersonic flow of air past rectangular cavities cut into a flat surface were studied. The cavities were found to emit a strong acoustic radiation. These acoustic fields were investigated by means of schlieren observation, interferometry, and hot-wire anemometer.
The frequency of the sound, as measured by a hot-wire, at a fixed depth of the gap was found to be inversely proportional to the breadth. No simple relationship was noticed between the Mach number M and a non dimensional frequency S based on the gas breadth and the free-stream velocity.
The intensity of the radiation was conveniently measured by means of an optical interferometer of the Mach-Zehnder type. At a Mach number of 0.8, a unit fringe shift was found to correspond to an intensity level of 160 decibels. Fringe shifts equal to and greater than 1 were observed for the radiations from these cavities, indicating that the acoustic fields were very intense.
languageEnglish
titleNACA-TN-3487num
titleAcoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfacesen
typestandard
page36
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext


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