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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F10%3A%230000998%21RIV11-MSM-00010669
rdf:type
n12:Vysledek skos:Concept
dcterms:description
This article deals with aerodynamic measurement of oscillated wing model AS28 with newly installed surface pressure transducers KULITE. In the frame of this work the practical task of the test of new technology of the surface pressure measurement and verifying of early results measured on this model was realized. There is introduced the development of unsteady measurement on the oscillated half-wing model in high speed laboratory of VZLU, the measurement, results and comparison of used methods. This article deals with aerodynamic measurement of oscillated wing model AS28 with newly installed surface pressure transducers KULITE. In the frame of this work the practical task of the test of new technology of the surface pressure measurement and verifying of early results measured on this model was realized. There is introduced the development of unsteady measurement on the oscillated half-wing model in high speed laboratory of VZLU, the measurement, results and comparison of used methods.
dcterms:title
Wind tunnel tests of oscillating wing using the surface pressure transducers. Wind tunnel tests of oscillating wing using the surface pressure transducers.
skos:prefLabel
Wind tunnel tests of oscillating wing using the surface pressure transducers. Wind tunnel tests of oscillating wing using the surface pressure transducers.
skos:notation
RIV/00010669:_____/10:#0000998!RIV11-MSM-00010669
n4:aktivita
n15:Z
n4:aktivity
Z(MSM0001066902)
n4:cisloPeriodika
4
n4:dodaniDat
n8:2011
n4:domaciTvurceVysledku
n9:7983433 n9:4954610 n9:5514258
n4:druhVysledku
n5:J
n4:duvernostUdaju
n17:S
n4:entitaPredkladatele
n10:predkladatel
n4:idSjednocenehoVysledku
298855
n4:idVysledku
RIV/00010669:_____/10:#0000998
n4:jazykVysledku
n11:eng
n4:klicovaSlova
high speed aerodynamics; unsteady pressure measurement; compressible flow; harmonic oscillation; transfer function
n4:klicoveSlovo
n6:high%20speed%20aerodynamics n6:compressible%20flow n6:harmonic%20oscillation n6:transfer%20function n6:unsteady%20pressure%20measurement
n4:kodStatuVydavatele
CZ - Česká republika
n4:kontrolniKodProRIV
[0C264E47AF92]
n4:nazevZdroje
Czech Aerospace Proceedings / Letecký zpravodaj
n4:obor
n7:JU
n4:pocetDomacichTvurcuVysledku
3
n4:pocetTvurcuVysledku
3
n4:rokUplatneniVysledku
n8:2010
n4:svazekPeriodika
4/2010
n4:tvurceVysledku
Benetka, Jiří Němec, Martin Vacek, Maxim
n4:zamer
n16:MSM0001066902
s:issn
1211-877X
s:numberOfPages
4