14.2845% 1917 0.869273 1.150386 16.6637% 1916 0.046449 21.528990 20.0069% 1915 0.668986 1.494801 9.1939% 1914 0.039872 25.080034 2.3510% 1913 0.072401 13.811889 1.1940% 1912 1.150669 0.869060 -1.1800% 1875 1.250000 0.800000 1.1940% 1912 0.061635 16.224649 1.1977% 1911 0.167682 5.963658 2.4765% 1910 0.203506 4.913850 3.8464% 1908
aerodynamically