Determination of indicial lift and moment of two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for mach number of 0.7.
Determination of indicial lift and moment of two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for mach number of 0.7
NACA -- Tech Note
1952
30 pages
Illustrations, Charts, Tables.
Report
English
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