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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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