A golf ball with aerodynamic coefficient magnitude and aerodynamic force angle, resulting in improved flight performance, such as increased carry and flight consistency regardless of ball orientation. In particular, the present invention is directed to a golf ball having increased flight distance as defined by a set of aerodynamic requirements at certain spin ratios and Reynolds Numbers, and more particularly the golf ball has a low lift coefficient at a high Reynolds Number.
CROSS-REFERENCE TO RELATED APPLICATIONS
This application is a continuation of U.S. patent application Ser. No. 11/607,916, filed Dec. 4, 2006, now abandoned, which is a continuation of U.S. patent application Ser. No. 10/784,744, filed Feb. 24, 2004, now U.S. Pat. No. 6,913,550, which is a continuation of U.S. patent application Ser. No. 10/096,852, filed Mar. 14, 2002, now U.S. Pat. No. 6,729,976, which is a continuation-in-part of U.S. patent application Ser. No. 09/989,191, filed Nov. 21, 2001, now U.S. Pat. No. 6,796,912, and also a continuation-in-part of U.S. patent application Ser. No. 09/404,164, filed Sep. 27, 1999, now U.S. Pat. No. 6,358,161, which is a divisional of U.S. patent application Ser. No. 08/922,633, filed Sep. 3, 1997, now U.S. Pat. No. 5,957,786. The entire disclosures of the related applications are incorporated by reference herein.
