Effect of mach number, Reynolds number, and thickness ratio on the aerodynamic characteristics of naca 63A-series airfoil sections.
Contributors: Gorenberg, N. B.
Series: Usaaml technical report -- 65-28
Publisher: U. A. Army Aviation Materiel Laboratories
Published: 1965
Place of publication: Fort Eustis, Virginia
Language: eng
Number of pages: 464