Helpful geometry visualization files
Download Matlab GTS file viewer
Download Matlab hermite file viewer
Boeing 747 Wire-frame input
Download B-747 hermite file
Boeing 747 Triangulated output from Trisurf
Download B-747 GTS file
Trigulated Friction analysis based on actual wetted areas
Mach Number = 0.85
Altitude = 30000 feet
Cd due to friction = 16.801 with Reference Area = 1 Sq. ft
No Wave drag analysis or Hypersonic Analysis since the configuration travels at high subsonic speeds
Approximate F16 aircraft
Download F16 Hermite file
Triangulated F16
Download F16 GTS file
Trigulated Friction analysis based on actual wetted areas
Mach Number = 1.4
Altitude = 30000 feet
Cd due to friction = 2.824 with Reference Area = 1 Sq. ft
Cd due to shock waves = 6.686 with Reference Area = 1 Sq. ft
A random aircraft
Download sample aircraft Hermite file
Triangulated sample aircraft
Download sample aircraft GTS file
Trigulated Friction analysis based on actual wetted areas
Mach Number = 1.4
Altitude = 30000 feet
Cd due to friction = 6.6116 with Reference Area = 1 Sq. ft
Cd due to shock waves = 3.618 with Reference Area = 1 Sq. ft
BTW, TRIAERO is not perfect.
Please visit
this page to view some failed cases. This may be helpful in your debugging process.