![]() Ground-Air-Ground (GAG) Cycle: Aircraft Ultimate Loads – GAG Cycle ![]() Let me get into some of these load cases in this post.Īs a clarification first, could I be oversimplifying these load cases? Probably, but I believe I am not far from the general methodology for developing a majority of these load cases, used in part sizing and stress analysis. ![]() ![]() It is fair to say that before any design and sizing efforts are conducted on new or modified aircraft designs, it is critical to determine the entire loads envelope that the aircraft will be subjected to during its service life, the highest being aircraft ultimate loads. Military fighter/trainer and rotor craft are outside the scope of this discussion so we will mainly focus on passenger transport category aircraft, and specifically from a structures stand point. Click here to access pdf versions of the latest blog posts… We already briefly covered Limit and Ultimate Loads in a previous FAA regulation blog post. In this post, I would like to expand on that discussion and cover my thoughts on various aircraft ultimate loads, especially limit and ultimate loads on transport category airplanes as well as engine nacelles in general.
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