Boychuk I. Method of complex aerodynamic modeling of freely flying system "glider-engine"

Object is a orbital cycle aerodynamic UAVs, target is development of the method of complex aerodynamic modeling of the complete orbital cycle winged UAVs based on a spatial model of the unsteady aero gas dynamic " glider-engine", which is a closed-off by equations of start dynamics and free flying, the methods are numerical experiments, the novelty is the method of complex aerodynamic modeling of free system " glider-engine " based on a complex aero gas dynamic model supplemented by the introduction of the closing conditions in the form of equations of start dynamics and free flying, there are numerically obtained gasdynamic characteristics of unsteady three-dimensional gas-dynamic interactions in the system " glider-engine", the results are ensuring the implementation of new aerodynamic schemes UAV with engines of direct response and minimization of project resources and technical risk, industry is aviation and rocket science.