Development of radial turbines in low-power Gas-turbine engines-modeling of gasdynamic processes. This method is applied to the turbine
impeller prototype. The most loaded places
Design of Blade Joints with Turbine Impeller Disk of Low-Power Gas Turbine EngineThe problem of ensuring gas dynamic and strength parameters in
impellers of low-power gas turbine
Corrosive Fluid Effects on Volute Surface Roughness in Centrifugal Pumps: A Computational StudyKashif Abbas,
Afaque Ahmed Bhutto,
Abdulhalim Musa Abubakar,
Isa Umaru Usman,
Zakiyyu Muhammad Sarkinbaka,
Tahiru Saka,
Mazen Abdul- Jabbar Alhodali,
Mohamed Ellouze,
Кашиф Аббас,
Афаке Ахмед Бхутто,
Абдулхалим Муса Абубакар,
Иса Умару Усман,
Закию Мухаммад Саркинбака,
Тахиру Сака,
Мазен Абдул-Джаббар Алходали,
Мохамед Эллюз and roughness height (h) of 20–40 m, 2000 rpm, 144 m
3/h, 0 atm and 0.5 m, were respectively
specified as initial
Анализ напорной характеристики центробежных компрессорных рабочих колесГалеркин, Ю.Б.,
Дроздов, А.А.,
Рекстин, А.Ф.,
Солдатова, К.В.,
Galerkin, Yuri B.,
Drozdov, Alexander A.,
Rextin, Alexey F.,
Soldatova, Christina V.
on the
impeller Mach number. The characteristics of this stage and the design characteristics
of the series of 10