Effect of compressibility on the distribution of pressures over a tapered wing of NACA 230-series airfoil sections

Author: Pearson, E O , Jr
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1390
Link: https://digital.library.unt.edu/ark:/67531/metadc55450/

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