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contributor authorReddy, Sohail R.
contributor authorChitale, Janhavi
contributor authorDulikravich, George S.
date accessioned2022-02-05T22:15:59Z
date available2022-02-05T22:15:59Z
date copyright2/8/2021 12:00:00 AM
date issued2021
identifier issn0098-2202
identifier otherfe_143_04_041504.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277238
description abstractThis work quantifies the uncertainty in Stevens Mark VII Perceived Level of sonic booms due to uncertainties in atmospheric profiles. The influence of temperature, humidity, and wind profiles, at six cities around the globe, on the sonic boom loudness is calculated. The flow field around an aircraft was obtained by solving the three-dimensional (3D), compressible Euler equations using the UNS3D solver. The near-field pressure signature is then propagated through the atmosphere by solving the augmented Burgers equation using the sBOOM solver. The uncertainty is modeled using a nonintrusive polynomial chaos approach. A sensitivity analysis is performed to identify the altitude range and the atmospheric variable to which the Perceived Level is most sensitive. It was shown that the Perceived Level is not sensitive to any particular altitude but rather the atmospheric profiles. It was also seen that the Perceived Level is highly sensitive to humidity and temperature profiles and less sensitive to the wind profiles.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Atmospheric Uncertainties on Sonic Boom Perceived Level
typeJournal Paper
journal volume143
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4049688
journal fristpage041504-1
journal lastpage041504-12
page12
treeJournal of Fluids Engineering:;2021:;volume( 143 ):;issue: 004
contenttypeFulltext


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