Effects of Independent Variations of Mach Number and Reynolds Number on Maximum Lift Coefficients of Four NACA 6-Series Airfoil Sections.
Effects of independent variations of mach number and Reynolds number on maximum lift coefficients of four NACA 6-series airfoil sections
NACA -- Tech Note
1952
32 pages
Report
English
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Engineering Index Backfile | 1947
|Engineering Index Backfile | 1950
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