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Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Klyuchnikov A.
Elaboration and testing of the algorithm which ensures an achievement of minimal deviation angle of flying model’s main centroidal axis of inertia during her counterbalancing in a sole correction flatness
Filonova M.
Тhe analysis of dependence of durability, risk of accidents and efficiency of transportations on airplane construction weight
Boyko O.
Product innovation index determination in aerospace industry
Razzhevaykin D., Razzhevajkin D.
EXACT SOLUTIONS OF EQUATION OF PLASTICITY OF PLANE STRESS CONDITION
Senashov S., Burmak V., Senashov S., Burmak V.
DEVELOPING AND REFINING THE ALGORITHM OF SINGLE-PLANE DYNAMIC BALANCING OF A HIGH-SPEED FLYING PROTOTYPE
Klyuchnikov A.
MODELING OF PLASTIC FLOW BETWEEN RIGID PLATES APPROACHING TO A CONSTANT ACCELERATION
Senashov S., Filyushina E.
CAUCHY PROBLEM SOLUTION FOR A HYPERBOLIC SYSTEM OF THE HOMOGENEOUS 2-DIMENSIONAL QUASILINEAR EQUATIONS
Senashov S., Yakhno A.
NUMERICAL ALGORITHM FOR OPTIMIZATION OF A PROCESS OF CONICAL FLYING MODEL EQUILIBRATION ON A VERTICAL BALANCING STAND
Klyuchnikov A.
Analysis and optimization of the plane fleet usageon route networks of the airline
Boiko O., Utenkov P.
METHOD OF EXPANSION OF A RANGE OF MEASUREMENT OF AERODYNAMIC PARAMETERS OF FLIGHT OF A MANEUVERING PLANE
Oleynik A.
OPTIMAL SYSTEMS OF SUBALGEBRAS ADMITTED BY EQUATIONS OF PLASTICITY
Burmak V.
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