Автор туралы ақпарат

Modorskii, V. Ya.

Шығарылым Бөлім Атауы Файл
Том 60, № 1 (2017) Aircraft and Rocket Engine Design and Development A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
Том 60, № 3 (2017) Aircraft and Rocket Engine Theory Computation of design parameters influence on air injector fuel atomization