Russian Aeronautics (Iz VUZ)
A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results
A software package for computer-aided design analysis of thin-walled structures from composite materials
Application of the parameter-averaging method to calculations of gas ejectors with cylindrical mixing chambers
Characteristics of turbine cascade with the modified leading edge of a profile
Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame
Dynamics investigation of the two-channel automatic system controlling the mirror of aircraft-based surveillance-search system
Generalization of experimental data on two-phase critical efflux through axisymmetric channels
Investigation of gyroplane takeoff with the use of main rotor collective pitch
Microindentation of plasma zirconia-based thermal barrier coatings
Numerical simulation of a boiling up fluid flow in the variable cross-section channels
On choice of turbulence models and grid parameters for computation of flows in diffuser ducts
Optimization of a tool kit for machining by methods of graph theory
Peculiarities of heat transfer in the hemispherical recesses streamlined by a pulsating flow
Stress concentration in compressor blades at their damage by foreign objects
Theoretical investigation of the vortex zone structure between periodic flow rectangular cross-section turbulators placed on the surface