Erratum: “Theoretical Prediction of the Pressure Distribution on a Non-lifting, Thin Symmetrical Aerofoil at Various Transonic Speeds”

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  • Theoretical Prediction of the Pressure Distribution on a Non-lifting, Thin Symmetrical Aerofoil at Various Transonic Speeds

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Page<BR>548   The upper limit of the intergral in (3.2) should be read as x−m|y|.<BR>548   The lower limit of the intergrals with respect to t in (3.9)–(3.12) should be read as 1.<BR>549   The multiplication factor in front of the bracket [   ] in (3.15) should be read as 4t⁄πβ.<BR>557   The explanatory title of Fig. 9 should be read as Reduced pressure drag coefficient \barCd of a circular-arc aerofoil versus ξ∞.

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