DETERMINATION OF SPECIFIC LOAD ACTING ON THE WING IN FLIGHT OF UNMANNED AERIAL VEHICLES OF AIRCRAFT TYPE: DETERMINATION OF SPECIFIC LOAD ACTING ON THE WING IN FLIGHT OF UNMANNED AERIAL VEHICLES OF AIRCRAFT TYPE

Хуснутдинова, Х.Х., Абдужабаров, Н.А., Тахиров, Ж.К.

Темир йўл транспорти: долзарб масалалар ва инновациялар · 2025-yil

Annotatsiya

This article discusses methods for determining the specific wing load of a UAV in flight. Two main methods are presented: the first is calculating the specific load during landing; the second is determining the specific load at cruising speed. The article also presents calculations for selecting engines, floats and batteries for vertical and horizontal flights. The selected components will improve the energy efficiency of the UAV, minimize weight and increase flight range. This development is aimed at optimizing the UAV design and improving their aerodynamic characteristics, which is important for increasing flight efficiency. 

Maqola ma’lumotlari
MualliflarХуснутдинова, Х.Х., Абдужабаров, Н.А., Тахиров, Ж.К.
JurnalТемир йўл транспорти: долзарб масалалар ва инновациялар
Nashr sanasi2025-02-17
Jild4
Betlar197-202
TilIngliz

Kalit so‘zlar

БПЛА, удельная нагрузка, время полета, крыло, статическая мощность, динамический анализ, конструктивные особенности., UAV, specific load, flight time, wing, static power, dynamic analysis, design features.

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