
The paper presents an analysis of research in optimal distribution of the airscrew thrust and the jet thrust of the turboprop engine. A conclusion is made as to the necessity of evaluating the efficiency of the power plant being a part of the aircraft.
Проведён анализ научных работ по оптимальному распределению тяги воздушного винта и реактивной тяги турбовинтового двигателя. Сделан вывод о необходимости оценки эффективности силовой установки в системе летательного аппарата.
ТУРБОВИНТОВОЙ ДВИГАТЕЛЬ, СКОРОСТЬ ИСТЕЧЕНИЯ, РАСПРЕДЕЛЕНИЕ ЭНЕРГИИ, ОПТИМИЗАЦИЯ, ОТНОСИТЕЛЬНАЯ МАССА, МОДЕЛИ МАССЫ
ТУРБОВИНТОВОЙ ДВИГАТЕЛЬ, СКОРОСТЬ ИСТЕЧЕНИЯ, РАСПРЕДЕЛЕНИЕ ЭНЕРГИИ, ОПТИМИЗАЦИЯ, ОТНОСИТЕЛЬНАЯ МАССА, МОДЕЛИ МАССЫ
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