We perform preliminary and certification loads analysis for part 23 aircraft. Based on lifting line theory, classical methods from NACA, Roskam and Torenbeek and approved methods from the part 23 regulations.
Comprehensive aircraft balanced load cases.
Nodal loads for finite element models.
Load envelopes and load loop comparisons.
We perform preliminary and certification loads analysis for part 23 aircraft. Based on lifting line theory, classical methods from NACA, Roskam and Torenbeek and approved methods from the part 23 regulations.
Comprehensive aircraft balanced load cases.
Nodal loads for finite element models.
Load envelopes and load loop comparisons.