Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4 Page: 1 of 112
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zTECHNICAL NOTE 3831
TABULATION OF MASS-FLOW PARAMETERS FOR USE IN DESIGN
OF TURBOMACHINE BLADE ROWS FOR RATIOS OF SPECIFIC
HEATS OF 1.3 AND 1.4
By Warren J. Whitney
Lewis Flight Propulsion Laboratory
Cleveland, Ohio
NACA
Washington
October 1956
AEi CNATIONAL ADVISORY COMMITTEE
FOR AERONAUTICSi
JtI-i
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Whitney, Warren J. Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4, report, October 1956; (https://digital.library.unt.edu/ark:/67531/metadc56065/m1/1/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.