6 Artículos
Acceso abierto | 08 oct 2021
Enhanced Feature Extraction Algorithms Using Oscillatory-Mode Pulsed Eddy Current Techniques for Aircraft Structure Inspection
Iuliia Lysenko
Department of Non-Destructive Testing Instruments and Systems, Faculty of Instrumentation Engineering, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”Kyiv, Ukraine
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, Yurii Kuts
Department of Non-Destructive Testing Instruments and Systems, Faculty of Instrumentation Engineering, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”Kyiv, Ukraine
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, Anatoliy Protasov
Department of Non-Destructive Testing Instruments and Systems, Faculty of Instrumentation Engineering, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”Kyiv, Ukraine
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, Mykhailo Redka
Department of Non-Destructive Testing Instruments and Systems, Faculty of Instrumentation Engineering, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”Kyiv, Ukraine
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y Valentin Uchanin
Karpenko Physico-Mechanical Institute of the National Academy of Sciences of UkraineLviv, Ukraine
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Acceso abierto | 08 oct 2021
Numerical Investigation of Detonation Propagation Through Small Orifice Holes
Ashish Vashishtha
Department of Aerospace Mechanical and Electronics Engineering, Institute of Technology CarlowIreland
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, Dean Callaghan
The Centre for Research and Enterprise in Engineering (engCORE), Institute of Technology CarlowIreland
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, Cathal Nolan
Department of Aerospace Mechanical and Electronics Engineering, Institute of Technology CarlowIreland
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y Acceso abierto | 08 oct 2021
Numerical Simulation of the Exit Temperature Pattern of an Aircraft Engine Using a Temperature-Dependent Turbulent Schmidt Number
, y Acceso abierto | 08 oct 2021
Impact of Load Retention on Aircraft Engine Parts Under Real Flight Cycle Conditions in Service Life Monitoring
Sergiy Yepifanov
Department of Aircraft Engine Design, Faculty of Aviation Engines, National Aerospace University “Kharkiv Aviation Institute”Kharkiv, Ukraine
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y Andrii Brunak
Department of Aircraft Engine Design, Faculty of Aviation Engines, National Aerospace University “Kharkiv Aviation Institute”Kharkiv, Ukraine
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Acceso abierto | 08 oct 2021
A Mathematical Model for Controlling a Quadrotor UAV
, y Acceso abierto | 08 oct 2021
A Two-Point Approximation Approach to Determining Aircraft Aerodynamic Force Coefficients for a Maximal-Duration Horizontal Flight
Andriy Viktorovich Goncharenko
National Aviation University, Aerospace Faculty,1, Liubomyra Huzara AvenueKyiv, Ukraine
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