Application of the Thin-Wing-Expansion Method to the Flow of a Compressible Fluid past a Symmetrical Circular Arc Aerofoil

抄録

In equation (5.10) on page 487,
eleventh line from the bottom   (4/3π³){2(1+····
should be   (4/3π³){4(1+····
seventh line from the bottom   ····+6ν²}[····
should be   ····+16ν²}[····
The author is indebted to Dr. John R. Spreiter for pointing out these errors. They are mistakes in printing and the numerial results in § 6 are not affected by these errors.