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Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Kornev A., Sereda V., Migalin K.
Thermal radiation of heterogeneous combustion products at the nozzle exit of the rocket microengine
Kuz’min V., Maratkanova E., Zagrai I., Rukavishnikova R.
Analysis of a beam with a crack under irregular cyclic load
Kayumov R., Mukhamedova I., Tuisina E.
An Integral Method of Surface Damping of Bending Vibrations for Thin-Walled Structures
Paimushin V., Firsov V., Shishkin V.
Study of flame stabilization in a model gas turbine combustor
Mingazov B., Baklanov A.
Hyperbolic Paraboloid for a Ruled Preform of an X-Fitting: Calculation of Parameters
Khaliulin V., Savitskii V., Zhukov A., Gimadiev R.
Simulation of thermal radiation emitted by heterogeneous combustion products in the combustion chamber of a model engine
Kuz’min V., Maratkanova E., Zagrai I., Rukavishnikova R.
Numerical Research of Intra-Chamber Transient Processes Dynamics during Starting Operation of the Solid Propellant Rocket Engine with Special Arrangement
Egorov M.
Studies of the screening surface proximity on integral aerodynamic characteristics of rectangular high-lift wings of different aspect ratio
Bukanov K., Zherekhov V.
Computation of design parameters influence on air injector fuel atomization
Sipatov A., Modorskii V., Babushkina A., Kolodyazhnyi D., Nagornyi V.
A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber
Baklanov A., Neumoin S.
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