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contributor authorBrown, Winfield James
contributor authorMcFadden, James D.
contributor authorMason, Howard J.
contributor authorTravis, Charles W.
date accessioned2017-06-09T17:32:49Z
date available2017-06-09T17:32:49Z
date copyright1974/02/01
date issued1974
identifier issn0021-8952
identifier otherams-8705.pdf
identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4230678
description abstractAnalysis of the frequency response of the input parameters of a gust probe system, which measures the turbulent flow of air, is presented. The results show that the system is very sensitive to noise created by aircraft structural and power plant vibrations. This noise appears in the form of discrete frequencies in the range 10 to 50 Hz. The noise may account for as much as 97% of the total power output by certain sensors. Since the usual range of interest for the measurement of fluctuations of meteorological parameters is 0 to 10 Hz, aliasing of these discrete frequencies may become a problem. This analysis is intended to characterize the noise so that some justification may be given to eliminate it from useful, significant data.
publisherAmerican Meteorological Society
titleAnalysis of the Research Flight Facility Gust Probe System
typeJournal Paper
journal volume13
journal issue1
journal titleJournal of Applied Meteorology
identifier doi10.1175/1520-0450(1974)013<0156:AOTRFF>2.0.CO;2
journal fristpage156
journal lastpage167
treeJournal of Applied Meteorology:;1974:;volume( 013 ):;issue: 001
contenttypeFulltext


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