, НАУ, кафедра авіаційних двигунів
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Proceedings of National Aviation University Vol. 26 No. 4 (2005) - MODERN AVIATION AND SPACE TEHNOLOGY
Profitability of the gas-turbine engine with two-row blade wreaths in the axial compressor
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Proceedings of National Aviation University Vol. 26 No. 4 (2005) - MODERN AVIATION AND SPACE TEHNOLOGY
The experimental stand for research turbomachine cascades
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Proceedings of National Aviation University Vol. 26 No. 4 (2005) - MODERN AVIATION AND SPACE TEHNOLOGY
Comparison of calculation methods of aviation gas-turbine engines turbine disc deformed state evaluation
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Proceedings of National Aviation University Vol. 27 No. 1 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Optimization parameters system maintenance transport aircraft
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Proceedings of National Aviation University Vol. 27 No. 1 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Simulation mechanism oscillations pressure vibration burning in low emission combustion chamber gas-turbine units
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Proceedings of National Aviation University Vol. 27 No. 1 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Сhoosing the best type neural network jet contour diagnostics engines
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Proceedings of National Aviation University Vol. 27 No. 1 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Сomplex and protection vibrokontrolyu gas compressor units "visa-pc"
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Proceedings of National Aviation University Vol. 28 No. 2 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Effect of geometrical characteristics input device gas turbine engine parameters on current
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Proceedings of National Aviation University Vol. 28 No. 2 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Problems of modern systems of logistical support in civil aviation
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Proceedings of National Aviation University Vol. 30 No. 4 (2006) - ENVIRONMENT PROTECTION
Method of calculating the depth of immersion of sea power station with an increase in height of the waves
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Proceedings of National Aviation University Vol. 30 No. 4 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Automated information-diagnostic system operational assessment of the degree of fuel injectors zakoksuvannya gas turbine engines
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Proceedings of National Aviation University Vol. 30 No. 4 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Evaluating the effectiveness of trend analysis algorithms for diagnosing turbine engine
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Proceedings of National Aviation University Vol. 30 No. 4 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Impulse technology for micro coating of titanium nitride at the end of compressor blades
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Proceedings of National Aviation University Vol. 31 No. 1 (2007) - MODERN AVIATION AND SPACE TEHNOLOGY
Determination of vibration characteristics of blades of gas turbine engines contactless method
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Proceedings of National Aviation University Vol. 30 No. 4 (2006) - MODERN AVIATION AND SPACE TEHNOLOGY
Determine the degree of degradation of the technical state of turbojet engines with double mixing flows in operating conditions
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