The historical development of NACA airfoils is briefly reviewed. Recent information of the aerodynamic characteristics of NACA airfoils is presented. This study, TR-824, was likewise effectively a catalog of NACA airfoil research, its authors noting (with justifiable pride) that Most useful of all NACA reports, and one that likewise became a standard reference for use by designers and other aeronautical engineers in airplane airfoil/wing design, was its effective replacement prepared in 1945 by Ira H. By 1945, as valuable as TR-460 had been, it was now outdated. The Agency, of course, continued its airfoil research in the 1930s, making notable advances in the development of high-speed airfoil sections and low-drag and laminar sections as well. Pinkerton, this document, TR-460, became a standard industry reference both in America and abroad. In the early 1930s, largely thanks to the work of Munk, the NACA had risen to world prominence in airfoil design, such status evident when, in 1933, the Agency released a report cataloging its airfoil research and presenting a definitive guide to the performance and characteristics of a wide range of airfoil shapes and concepts. X-15 THE WORLD'S FASTEST ROCKET PLANE AND.Praxis Manned Spaceflight Log 1961-2006.HEINKEL Chronik und Typenblatter der Firmo Heinkel-Flugzeugbau.Facing the Heat Barrier: a History of Hypersonics.
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