panel code การใช้

• An intermediate step between Panel Codes and Full Potential codes were codes that used the Transonic Small Disturbance equations.
• In the two-dimensional realm, a number of Panel Codes have been developed for airfoil analysis and design.
• Both PROFILE and XFOIL incorporate two-dimensional panel codes, with coupled boundary layer codes for airfoil analysis work.
• The first lifting Panel Code ( A230 ) was described in a paper written by Paul Rubbert and Gary Saaris of Boeing Aircraft in 1968.
• In time, more advanced three-dimensional Panel Codes were developed at Boeing ( PANAIR, A502 ), Douglas ( HESS ), McDonnell Aircraft ( MACAERO ), NASA ( PMARC ) and Analytical Methods ( WBAERO, USAERO and VSAERO ).