Transonic Compressor Test Rig rebuild and initial results with the Sanger stage

Transonic Compressor Test Rig rebuild and initial results with the Sanger stage

Approved for public release; distribution is unlimited === The NPS Transonic Compressor Test Rig was rebuilt and initial testing was conducted on the Sanger Stage, which was designed using CFD techniques. Improvements to the existing monitoring equipment, test rig instrumentation, and data acquisiti...

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Bibliographic Details
Main Author: O'Brien, Joseph Morton
Other Authors: Shreeve, Raymond P.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/7813
id ndltd-nps.edu-oai-calhoun.nps.edu-10945-7813
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-78132015-08-06T16:02:57Z Transonic Compressor Test Rig rebuild and initial results with the Sanger stage O'Brien, Joseph Morton Shreeve, Raymond P. Hobson, Garth Approved for public release; distribution is unlimited The NPS Transonic Compressor Test Rig was rebuilt and initial testing was conducted on the Sanger Stage, which was designed using CFD techniques. Improvements to the existing monitoring equipment, test rig instrumentation, and data acquisition software were all made in preparation for testing. A Plexiglas casewall was chosen to accommodate pressure-sensitive paint measurements. Wall heating was used to control tip-clearance. The initial performance data, to 70% design speed, were compared with predictions using a 3-dimensional viscous code 2012-08-09T18:48:22Z 2012-08-09T18:48:22Z 2000-06 Thesis http://hdl.handle.net/10945/7813 en_US Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description Approved for public release; distribution is unlimited === The NPS Transonic Compressor Test Rig was rebuilt and initial testing was conducted on the Sanger Stage, which was designed using CFD techniques. Improvements to the existing monitoring equipment, test rig instrumentation, and data acquisition software were all made in preparation for testing. A Plexiglas casewall was chosen to accommodate pressure-sensitive paint measurements. Wall heating was used to control tip-clearance. The initial performance data, to 70% design speed, were compared with predictions using a 3-dimensional viscous code
author2 Shreeve, Raymond P.
author_facet Shreeve, Raymond P.
O'Brien, Joseph Morton
author O'Brien, Joseph Morton
spellingShingle O'Brien, Joseph Morton
Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
author_sort O'Brien, Joseph Morton
title Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
title_short Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
title_full Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
title_fullStr Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
title_full_unstemmed Transonic Compressor Test Rig rebuild and initial results with the Sanger stage
title_sort transonic compressor test rig rebuild and initial results with the sanger stage
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/7813
work_keys_str_mv AT obrienjosephmorton transoniccompressortestrigrebuildandinitialresultswiththesangerstage
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