Keyword: «landing at refusal of two engines»

AERODYNAMIC SUBSTANTIATION AND THE ANALYSIS OF BEHAVIOUR OF THE HELICOPTER AT PARTIAL REFUSAL OF TWO ENGINES AT FLIGHT AT IS LIMITING-SMALL HEIGHT

Authors:

Pyotr Vasilev,

Vadim Popov

In article modern ways of performance of flights on fighting application are considered provide use of is limiting-small heights (ПМВ).

Keywords: crew, the helicopter, the aviation technics, landing at refusal of two engines, flight at is limiting-small height, prelanding maneuver