Numerical simulation of an explosion in the air using a high-order approximation difference scheme
Authors: Menshakov S.S., Taran V.A.
Issue: #5 (161)
Mechanics
Aviation and Rocket-Space Engineering
Flow peculiarities in the bottom region of experimental aircraft models
Authors: Sidnyaev N.I., Battulga Enkhjargal
Analysis and improvement of calculation of parameters of free gas flow around a vertical plate or cylinder to be used when studying aircraft thermal conditions at the launch complex
Authors: Barmin I.V., Romanyak A.Yu., Matveeva O.P.
Computational study of the pin nozzle geometry and the flight conditions influence on the thrust characteristics
Authors: Taran K.A., Fedotova K.V.
Profiling the surface of the nozzle unit sealing insert of an axial turbine with the regulated nozzle set
Authors: Shemetovets A.A., Nesterenko V.G.
Computational experimental assessment of the optimization algorithm for the inertial platform initial alignment
Authors: Naumchenko V.P.
Criteria for selective choice of the most reliable information source in measurement systems
Authors: Radyukin A.Yu., Maslennikov A.L.