&lt;title&gt;Built-in fiber sensors for safe use of aircraft&lt;/title&gt;

Pol'ski, Yuri E.; Morozov, Oleg G.

doi:10.1117/12.259095

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“…Distributions of pressure and velocity throughout the cantilever obtained at conditions of channel flow action are calculated by using the finite-element method; the background noises are in this case ignored; as a result, it made it possible to determine the non-uniformities of the noise structure of reactive gas flow at the nozzle section more exactly [10][11][12][13][14] . At the same time, it is possible to determine the presence of typical or uncertain defects by using as the base the deviations of frequency levels of acoustic pressure from the reference ones.…”

Section: The Principles Of Passive Spatial Locations Of Defects On a mentioning

confidence: 99%