Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading Page: 1 of 29
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RM E54F14C
RESEARCH MEMORANDUM
EXPERIMENTAL DETERMINATION OF AERODYNAMIC FORCES
NORMAL TO THE CHORD DUE TO ROTATING STALL
ACTING ON COMPRESSOR BLADING
By Donald F. Johnson and Eleanor L. Costilow
Lewis Flight Propulsion Laboratory
Cleveland, Ohio
CLASSIFICATTON CHITi.& -- _
To. UCLASSIFIU , . . .
This satrlaL contains liformtiona inft tl Ntsionnal Defense t s United sSthe t mning
of th e eAcags lawn , Title 18, U.S.C., BSeca. 9 and ?S , the tramiseln or revebtios of which In any
nar to an unnthrfled peron is prohibited by lw.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
1 WASHINGTON
August 24, 1954
S~'~ i~~b
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Johnson, Donald F. & Costilow, Eleanor L. Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading, report, August 24, 1954; (https://digital.library.unt.edu/ark:/67531/metadc64836/m1/1/: accessed April 20, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.