Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections / by E.O. Pearson, Jr., A.J. Evans and F.E.West, Jr 1945 [LeatherBound]

E. O Pearson

Publication Date: 2025
Language: English
Condition: New Hardcover

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