Abstract The informative aerometric parameters of the helicopter main rotor vortex column, the approaches to their description and perception, the mathematical models of algorithms for determining helicopter altitude-speed parameters using the aerometric information from the vortex column are considered.
Methodological foundations for helicopter altitude-speed parameter measurement using aerometric information from the main rotor vortex column
Russian Aeronautics (Iz VUZ) ; 53 , 3 ; 320-327
2010-09-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch