RTU Research Outputs and Resources: Reasearch Staff

Experience of Applying the Acoustic Emission Method for Monitoring Systems
(2024)

Leonīds Vinogradovs, Aleksejs Nasibullins, Mukharbiy Banov, Jūlija Soldatova, Juris Gutāns
Publication (anonimusly reviewed) in a journal with an international editorial board indexed in other databases

Research on Fatigue Fracture Kinetics of Helicopter Fuselage Bolting Elements
(2016)

Aleksandrs Urbahs, Kristīne Carjova, Aleksejs Nasibullins, Jurijs Feščuks
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

Optimization of Hybrid Joints for Improving Their Reliability
(2014)

Alexander Arnautov, Viktor Gribniak, Ilmārs Blumbergs, Māris Hauka, Aleksejs Nasibullins
Conference paper

Design of Adhesive Joints with Different Elastic Properties
(2014)

Māris Hauka, Aleksejs Nasibullins, Ilmārs Blumbergs, Viktor Gribniak, Oskars Bikovens, Jevgenija Ponomarenko
Conference paper

Analysis of the Mechanism of Destruction of Aircraft Components
(2013)

Aleksandrs Urbahs, Mukharbiy Banov, Aleksejs Nasibullins, Kristīne Carjova
Publication (anonimusly reviewed) in a journal with an international editorial board indexed in other databases

Using Acoustic Emission Method during Bench-Tests of Load-Bearing Aviation Units
(2011)

Aleksejs Nasibullins
Doctoral Thesis

Acoustic Emission Characteristics of Fatigue Crack Development in a Pitch Control Arm of Helicopter Lifting Propeller Blades
(2010)

Aleksejs Nasibullins, Jevgēņijs Garbuzs, Sergejs Doroško
Full-text conference paper published in other conference proceedings

Using Acoustic Emission Method When Carrying out Fatigue Tests of Pitch Arm of EH-101 Helicopter
(2010)

Aleksejs Nasibullins
Publications in RTU scientific journal

Acoustic Emission Monitoring of Fatigue Crack Origination during Titanium Specimens Tests
(2010)

Aleksejs Nasibullins, Aleksandrs Urbahs, Mukharbiy Banov
Publications in RTU scientific journal

The Helicopter’s MI-26T Tail and Fin Booms Stressed State under Static Loading
(2009)

Aleksejs Nasibullins, Vladislav Turko
Scientific article indexed in ERIH database, in INT1 or INT2 category journals

Information about Author

Publications

Experience of Applying the Acoustic Emission Method for Monitoring Systems
(2024)

Research on Fatigue Fracture Kinetics of Helicopter Fuselage Bolting Elements
(2016)

Optimization of Hybrid Joints for Improving Their Reliability
(2014)

Design of Adhesive Joints with Different Elastic Properties
(2014)

Analysis of the Mechanism of Destruction of Aircraft Components
(2013)

Using Acoustic Emission Method during Bench-Tests of Load-Bearing Aviation Units
(2011)

Acoustic Emission Characteristics of Fatigue Crack Development in a Pitch Control Arm of Helicopter Lifting Propeller Blades
(2010)

Using Acoustic Emission Method When Carrying out Fatigue Tests of Pitch Arm of EH-101 Helicopter
(2010)

Acoustic Emission Monitoring of Fatigue Crack Origination during Titanium Specimens Tests
(2010)

The Helicopter’s MI-26T Tail and Fin Booms Stressed State under Static Loading
(2009)

Patents

Method for evaluation of fatigue crack growth during cyclic load testing of construction
LV13853B (20.04.2009.)

Information about Author

Publications

Experience of Applying the Acoustic Emission Method for Monitoring Systems (2024)

Research on Fatigue Fracture Kinetics of Helicopter Fuselage Bolting Elements (2016)

Optimization of Hybrid Joints for Improving Their Reliability (2014)

Design of Adhesive Joints with Different Elastic Properties (2014)

Analysis of the Mechanism of Destruction of Aircraft Components (2013)

Using Acoustic Emission Method during Bench-Tests of Load-Bearing Aviation Units (2011)

Acoustic Emission Characteristics of Fatigue Crack Development in a Pitch Control Arm of Helicopter Lifting Propeller Blades (2010)

Using Acoustic Emission Method When Carrying out Fatigue Tests of Pitch Arm of EH-101 Helicopter (2010)

Acoustic Emission Monitoring of Fatigue Crack Origination during Titanium Specimens Tests (2010)

The Helicopter’s MI-26T Tail and Fin Booms Stressed State under Static Loading (2009)

Patents

Method for evaluation of fatigue crack growth during cyclic load testing of construction LV13853B (20.04.2009.)

Experience of Applying the Acoustic Emission Method for Monitoring Systems
(2024)

Research on Fatigue Fracture Kinetics of Helicopter Fuselage Bolting Elements
(2016)

Optimization of Hybrid Joints for Improving Their Reliability
(2014)

Design of Adhesive Joints with Different Elastic Properties
(2014)

Analysis of the Mechanism of Destruction of Aircraft Components
(2013)

Using Acoustic Emission Method during Bench-Tests of Load-Bearing Aviation Units
(2011)

Acoustic Emission Characteristics of Fatigue Crack Development in a Pitch Control Arm of Helicopter Lifting Propeller Blades
(2010)

Using Acoustic Emission Method When Carrying out Fatigue Tests of Pitch Arm of EH-101 Helicopter
(2010)

Acoustic Emission Monitoring of Fatigue Crack Origination during Titanium Specimens Tests
(2010)

The Helicopter’s MI-26T Tail and Fin Booms Stressed State under Static Loading
(2009)

Method for evaluation of fatigue crack growth during cyclic load testing of construction
LV13853B (20.04.2009.)