Computational investigations of Ka-226T helicopter coaxial rotor aerodynamics in the vortex ring state

The vortex ring states are observed when the rotor is flowed at positive angles of attack. For the main rotor, these conditions are realized during a steep descent of the helicopter at low speeds. The rotor vortex ring states are affected by significant phenomena related to the behavior of its aerod...

Бүрэн тодорхойлолт

Номзүйн дэлгэрэнгүй

Үндсэн зохиолчид:	P. V. Makeev, Yu. M. Ignatkin, A. I. Shomov, S. V. Selemenev
Формат:	Artigo
Хэл сонгох:	Russo
Хэвлэсэн:	Moscow State Technical University of Civil Aviation 2024-05-01
Цуврал:	Научный вестник МГТУ ГА
Нөхцлүүд:	coaxial main rotor nonlinear vortex model hover steep descent vortex ring states aerodynamics boundaries of vortex ring states
Онлайн хандалт:	https://avia.mstuca.ru/jour/article/view/2338
Шошгууд:	Шошго нэмэх Шошго байхгүй, Энэхүү баримтыг шошголох эхний хүн болох!