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タイトルLanding Gear Components Noise Study - PIV and Hot-Wire Measurements
本文(外部サイト)http://hdl.handle.net/2060/20100012182
著者(英)Price, Jennifer L.; Burley, Casey L.; Becker, Lawrence E.; Stead, Daniel J.; Hutcheson, Florence V.
著者所属(英)NASA Langley Research Center
発行日2010-03-01
言語eng
内容記述PIV and hot-wire measurements of the wake flow from rods and bars are presented. The test models include rods of different diameters and cross sections and a rod juxtaposed to a plate. The latter is representative of the latch door that is attached to an aircraft landing gear when the gear is deployed, while the single and multiple rod configurations tested are representative of some of the various struts and cables configuration present on an aircraft landing gear. The test set up is described and the flow measurements are presented. The effect of model surface treatment and freestream turbulence on the spanwise coherence of the vortex shedding is studied for several rod and bar configurations.
NASA分類Acoustics
レポートNONASA/TM-2010-216209
NF1676L-10288
L-19839
権利Copyright, Distribution as joint owner in the copyright


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