Investigation of Aircrafts Landing Gear Configuration and Basic Design Requirements
محل انتشار: نوزدهمین کنفرانس بین المللی انجمن هوافضای ایران
سال انتشار: 1400
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 611
فایل این مقاله در 8 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
AEROSPACE19_099
تاریخ نمایه سازی: 10 دی 1400
چکیده مقاله:
Aircraft landing gear supports the entire weight of an aircraft during landing and ground operations. They are attached to primary structural members of the aircraft. The type of gear depends on the aircraft design and its intended use. Most landing gear have wheels to facilitate operation to and from hard surfaces, such as airport runways. Other gear feature skids for this purpose, such as those found on helicopters. In this article all Aircrafts Landing Gear Configuration and Basic Design Requirements has been investigated.
کلیدواژه ها:
landing gear configuration - aircraft design- aircraft structure- primary structural members
نویسندگان
Omid Habibi
M.S student of Aerospace Engineering, K. N. Toosi University of Technology,
MohammadMorteza Anbarlooei
PhD student of Aerospace Engineering, K. N. Toosi University of Technology,