1.
Stress Distribution Analysis using ANSYS of the Nose Landing Gear of STOL Aircrafts Considering Runway Gradient: A Simulation Study. Orchid Acad. Siraha [Internet]. 2023 Dec. 31 [cited 2026 Jul. 16];2(1):1-20. Available from: https://www.nepjol.info/index.php/oas/article/view/65618