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Numerical and experemental investigation of the dynamics of light multipurpose helicopter ditching
Mikhailov S.A., Nedelko D.V., Mukhametshin T.A., Belyaevskiy A.N., Gontsova L.G.
Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping
Onushkin Y.P., Sizov D.A., Poluyakhtov V.A., Ostrovoy A.V.
Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft
Mashoshin O.F., Semenikhin R.L.
Mathematical description of the interaction between a probing microwave signal and the helicopter main rotor blade
Danilin A.I., Zhukov S.V., Popov M.S.
Mathematical model of complex spatial deformation of rotor blades during helicopter arbitrary motion
Girfanov A.M.
Feature of optimization of parameters of working process GTE with the free turbine at initial designing in the conditions of uncertainty
1 1., 1 1.
Method of improving control using a simulation object model and its application to the problem of helicopter emergency landing manoeuvre optimization
Kvokov V.N., Trushkova Y.A., Ukhin M.Y.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
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