Show simple item record

contributor authorWatanabe, Toshinori
contributor authorAzuma, Toshihiko
contributor authorUzawa, Seiji
contributor authorHimeno, Takehiro
contributor authorInoue, Chihiro
date accessioned2019-02-28T11:10:00Z
date available2019-02-28T11:10:00Z
date copyright4/18/2018 12:00:00 AM
date issued2018
identifier issn0889-504X
identifier otherturbo_140_06_061003.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253377
description abstractA fast-response pressure-sensitive paint (PSP) technique was applied to the measurement of unsteady surface pressure of an oscillating cascade blade in a transonic flow. A linear cascade was used, and its central blade was oscillated in a translational manner. The unsteady pressure distributions of the oscillating blade and two stationary neighbors were measured using the fast-response PSP technique, and the unsteady aerodynamic force on the blade was obtained by integrating the data obtained on the pressures. The measurements made with the PSP technique were compared with those obtained by conventional methods for the purpose of validation. From the results, the PSP technique was revealed to be capable of measuring the unsteady surface pressure, which is used for flutter analysis in transonic conditions.
publisherThe American Society of Mechanical Engineers (ASME)
titleUnsteady Pressure Measurement on Oscillating Blade in Transonic Flow Using Fast-Response Pressure-Sensitive Paint
typeJournal Paper
journal volume140
journal issue6
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4039180
journal fristpage61003
journal lastpage061003-8
treeJournal of Turbomachinery:;2018:;volume 140:;issue 006
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record