Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading

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dc.contributor.authorSanger, N.L.
dc.contributor.authorShreeve, R.P.
dc.contributor.corporateGlenn Research Center
dc.dateJune 1986en_US
dc.date.accessioned2018-09-27T00:06:58Z
dc.date.available2018-09-27T00:06:58Z
dc.date.issued1986-06
dc.descriptionInternational Gas Turbine Conference and Exhibit; 8-12 Jun. 1986; Dusseldorf; Germanyen_US
dc.description.abstractThe mid-span section of a previously reported controlled-diffusion compressor stator has been experimentally evaluated in cascade. Measurements are taken over a range of incidence angles for blade chord Reynolds numbers from 470,000 to 690,000. Blade chord length is 12.7 cm, aspect ratio is 2.0, and solidity is 1.67. Measurements include conventional cascade performance parameters as well as blade surface pressures. Computations are made for the inviscid flow field, surface boundary layers, and loss for several of the blade inlet angle conditions, are compared against corresponding data.en_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.
dc.description.funderRTOP 505-62-21
dc.identifier.other19860006749
dc.identifier.otherNASA-TM-87167, E-2805, NAS 1.15:87167
dc.identifier.urihttps://hdl.handle.net/10945/60135
dc.identifier.urihttps://ntrs.nasa.gov/search.jsp?R=19860006749
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.subject.authorBOUNDARY LAYERSen_US
dc.subject.authorCASCADE FLOWen_US
dc.subject.authorCOMPARISONen_US
dc.subject.authorCOMPRESSOR BLADESen_US
dc.subject.authorCOMPRESSORSen_US
dc.subject.authorCOMPUTATIONen_US
dc.subject.authorDIFFUSIONen_US
dc.subject.authorEXPERIMENTATIONen_US
dc.subject.authorGAS TURBINE ENGINESen_US
dc.subject.authorINVISCID FLOWen_US
dc.subject.authorREYNOLDS NUMBERen_US
dc.subject.authorSTATORSen_US
dc.subject.authorSURFACE LAYERSen_US
dc.subject.authorASPECT RATIOen_US
dc.subject.authorCHORDS (GEOMETRY)en_US
dc.subject.authorPRESSUREen_US
dc.titleComparison of calculated and experimental cascade performance for controlled-diffusion compressor stator bladingen_US
dc.typeConference Paper
dspace.entity.typePublication
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