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Reconstruction of the Unsteady Pressure Field in a Low Speed Linear Cascade

Förster, Felix; Sims-Williams, David; Ingram, Grant

Authors

Felix Förster



Abstract

This paper describes investigations into unsteady flow phenomena in a high turning linear cascade with a nominal steady flow. A fast response five hole probe was used to obtain time-accurate measurements. Since a single probe was used to traverse an entire measurement plane, the results were obtained as discrete points and were not synchronous. One method used to address this issue is to traverse the measurement plane point by point and record the signal of a reference probe simultaneously. Synchronization can be performed during post processing by analyzing the reference signal for a common periodic component and phase-shifting all signals with respect to the reference phase of that flow feature. This paper presents results from the application this unsteady reconstruction technique to the so-called Durham Cascade 28% downstream of the trailing edge in order to provide insight into the nature of the dominant unsteady mode. It was found that there was significant temporal variation in the strength of the passage vortex but the position of the vortex remains fixed.

Citation

Förster, F., Sims-Williams, D., & Ingram, G. (2012). Reconstruction of the Unsteady Pressure Field in a Low Speed Linear Cascade. In ASME Turbo Expo 2012 : turbine technical conference and exposition (2653-2662). https://doi.org/10.1115/gt2012-69156

Presentation Conference Type Conference Paper (Published)
Conference Name ASME Turbo Expo 2012: Turbine Technical Conference and Exposition
Publication Date Jan 1, 2012
Deposit Date Aug 6, 2013
Publisher American Society of Mechanical Engineers
Volume 8
Pages 2653-2662
Series Title Turbomachinery, parts A, B, and C
Book Title ASME Turbo Expo 2012 : turbine technical conference and exposition
DOI https://doi.org/10.1115/gt2012-69156
Keywords Pressure , Cascades (Fluid dynamics)
Public URL https://durham-repository.worktribe.com/output/1155294
Additional Information Paper no: GT2012-69156