G.J. has developed proprietary computer programs that calculate basic dynamic properties, durable Damage Tolerance, Finite Element Modeling, vertical and lateral discrete and power spectral density gust loads, symmetric and anti-symmetric steady-state maneuver loads of an elastic airplane, static divergence, static aeroelastic corrections and control effectiveness, dynamic level landing loads with arbitrary input load time histories, and symmetric and anti-symmetric dynamic response of an elastic airplane resulting from arbitrary control inputs, vibrations, flutter, fatigue, performance, stability and control, flight analysis, and wind tunnel testing.