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Pesquisa

Edição
Título
Autores
Practice in the application of specialized technologic process patterns of 5-axis machining operation of blade rings of blisks
Khaimovich I., Surkov O., Khaimovich A.
Algorithm of Numerical Checking Calculation of Turbine Cooled Blades of Gas Turbine Engines Using Experimental Data on Heat Transfer and Resistance
Il’inkov A., Ermakov A., Takmovtsev V., Shchukin A., Erzikov A.
Disk wing to main rotor conversion mechanics
Pavlov V., Gasilov M.
Accounting for Geometric Scatter within Manufacturing Tolerances on the Natural Frequency Values of Compressor Rotor Blade during Its Detuning from Dangerous Resonances
Vasil’ev B., Semenov A., Sal’nikov A., Bortnikov A.
Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades
Berdin V., Smyslov A., Berdin N., Luk’yanov V.
Vortex Structure Intensity in Diffuser Dimples
Il’inkov A., Takmovtsev V., Shchukin A., Khabibullin I., Zaripov I.
Dynamics of Main Rotor to Disk Wing Conversion
Pavlov V., Gasilov M., Yusupov D.
Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
Kulikov G., Trushin V., Abdulnagimov A., Ganeev A.
Design of gating systems in production of gas turbine engine blades
Smykov A., Moiseev V., Chumadin A.
Development, research and production of a centrifugal impeller
Gureev V., Salakhov R., Falyakhov M., Kudusov D., Burlakov V.
Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties
Arkhipov A., Volgina M., Matushkin A., Ravikovich Y., Kholobtsev D.
Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
Remizov A., Vyatkov V., Lebedev V.
Study of Jet Propagation and Prevention of Jet Reattachment to the Nacelle during Jet Engine Thrust Reversal
Mikhailov A., Nasyrov S., Samerkhanov T., Kosterin A.
A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
Pavlov V.
Numerical and Experiment Investigation of the Friction Coefficient in Gas Turbine Impeller Dovetail Joints
Sapron D., Gukasyan S., Mezentsev M.
Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
Gorelov A., Nikolaev E., Sidorov I.
1 - 16 de 16 resultados
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