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Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
Arkhipov A., Volgina M., Matushkin A., Ravikovich Y., Kholobtsev D.
A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
Pavlov V.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Arkhipov A., Volgina M., Matushkin A., Ravikovich Y., Kholobtsev D.
Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Spatial vibration protection in a turbopump of hydrogen rocket engines
Belousov A., Ponomarev Y.
Numerical Analysis of Hovering Main Rotor Aero-Acoustic Characteristics for Ice Detection
Chen X., Zhao Q., Barakos G., Kusyumov A.
Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle
Grumondz V., Al’bokrinova A., Noskov S.
Numerical modeling of helicopter flight on a prescribed trajectory
Girfanov A., Girfanova R.
Optimization of the Stage Number and Parameter Distribution in the Flow Passage at GTE Compressor and Turbine Design
Krivosheev I., Rozhkov K., Simonov N.
Exploring the Detached-Eddy Simulation for Main Rotor Flows
Dehaeze F., Barakos G., Kusyumov A., Kusyumov S., Mikhailov S.
Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
Gorelov A., Nikolaev E., Sidorov I.
Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Influence of the Air Viscosity on the Induced Power of a Helicopter Main Rotor in Hover and Vertical Takeoff Modes
Shaidakov V., Brusov V.
Disk wing to main rotor conversion mechanics
Pavlov V., Gasilov M.
Problem of the Community Noise Reduction for Aircraft with Open Rotor Engines
Moshkov P., Samokhin V., Yakovlev A.
Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method
Aparinov A., Kritskii B., Setukha A.
Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
Ignatkin Y., Makeev P., Shomov A.
Study of the Radial Vibrations of a Rotor of a Leak-Proof Electric Pump Engine
Chernyshov M., Lekanov A., Razhikov V., Kholopov S.
Trends in research of hydrodynamic damping in rotor supports of gas turbine engines
Falaleev S.
Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
Nikolaev E., Nikolaeva M.
Study of the Local Strength of the Main Rotor Torsion Bar under the Action of Flight and Test Bench Loads
Mitryaikin V., Shuvalov V.
Development of wireless strain-gauge measurement system for structural tests
Uvarov M., Naumov V.
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