Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor With Two Transonic Inlet Stages 1: Aerodynamic Design Page: 1 of 37
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SECURITY Y INFORMV1AT ION
RM E5 324
..... . ..
INVESTIGATION OF A HIGH-PRESSURE-RATIO EIGHT-STAGE
AXIAL-FLOW RESEARCH COMPRESSOR WITH TWO
TRANSONIC INLET STAGES
I - AERODYNAMIC DESIGN
By Charles H. Voit
Lewis Flight Propulsion Laboratory
C leveland, Ohio
This aterial contasinformation affecting the National Defense of the United States within the meaning
of the espionage laws, Title 18, U.S.C., Secs. 7935 and 794, the transmission or revelation of which in sny
manner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
December 4, 1953RECEIPT SNATiRE
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Voit, Charles H. Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor With Two Transonic Inlet Stages 1: Aerodynamic Design, report, December 4, 1953; (digital.library.unt.edu/ark:/67531/metadc59882/m1/1/: accessed February 18, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.