NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Johns Hopkins University Stereoscopic Particle Image Velocimetry (SPIV) Test ResultsProfessor J. Katz at the Johns Hopkins University conducted an experimental investigation of the effect of varying the clearance over the tip of a compressor rotor in an embedded stage through a NASA funded award. The activity provided very detailed stereo Particle Image Velocimetry (PIV) measurements of the tip flow field in their optically index-matched facility. The researchers were able to measure and visualize the unsteady velocity and pressure field in the tip gap area for the first time from which they have published more than 10 Journal papers. The dataset has been used widely within NASA for internal program development. The compressor geometry is part of the NASA Low-Speed Axial Compressor (LSAC) compressor stage geometry which is publicly available. All the casing treatment geometries were published by the researchers at JHU. The PIV data has also been published in several ASME papers and presented at recent TurboExpo Conferences. Many research groups at universities and US industry would like access to this data; therefore, we would like to prepare the data package and release it to public. The data package will be announced on data.nasa.gov.
Document ID
20205002403
Acquisition Source
Glenn Research Center
Document Type
Other - Data package for public release
Authors
Barbara L Lucci
(Glenn Research Center Cleveland, Ohio, United States)
Chunill Hah
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 19, 2020
Publication Date
May 19, 2020
Publication Information
Subject Category
Aeronautics (General)
Funding Number(s)
WBS: 081876.02.03.04.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Compressor
Blade
Data
No Preview Available