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Charles H. Zimmerman
Charles Horton Zimmerman (1908 – 5 May 1996), was an aeronautical engineer, whose work on novel airfoil configurations led to several notable experimental aircraft programs.
==Early work==
Zimmerman worked at Langley Memorial Aeronautical Laboratory in the 1930s on a variety of research topics, including loads,〔M. J. Bamber and C. H. Zimmerman (1933) (''Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance'' ), NACA TN-474.〕〔M. J. Bamber and C. H. Zimmerman (1935) (''The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance'' ), NACA TN-517.〕〔M. J. Bamber and C. H. Zimmerman (1936) (''Spinning characteristics of wings I : rectangular Clark Y monoplane wing'' ), NACA TN-519.〕 airfoils,〔C. H. Zimmerman (1933) (''Characteristics of Clark Y airfoils of small aspect ratios'' ), NACA TN-431.〕〔C. H. Zimmerman (1935) (''Aerodynamic characteristics of several airfoils of low aspect ratio'' ), NACA TN-539.〕 and aircraft stability and design.〔C. H. Zimmerman (1936) (''An analysis of longitudinal stability in power-off flight with charts for use in design'' ), NACA TN-521.〕〔C. H. Zimmerman (1936) (''Effect of changes in tail arrangement upon the spinning of a low-wing monoplane model'' ), NACA TN-570.〕 During this time, he was also thinking about much more novel aspects of flight, especially how stability might be maintained. He theorized that the natural balancing reflexes of a person could be adequate to control very small flight vehicles, a concept he called "kinesthetic control". He was also interested in aspects that could lead to Vertical/Short Takeoff and Landing aircraft.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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