Transonic methods for most of the aerodynamic data do not exist. The recommended procedure requires fairing between subsonic and supersonic data using available data as a guide. Straight tapered, cranked,or double delta planforms are treated. Effects of sweep, taper and incidence are included. Linear twist is treated at subsonic Mach numbers.
Dihedral effects are present in the lateral directional data.
Lateral directional solutions consider high and low-wing positions. See table 2 in the printed version for full details. Wing downwash methods are restricted to straight tapered planforms. Effects of twin vertical tails are included in the static lateral directional data at subsonic Mach numbers. Strakes can be run via a double-delta wing.