FLOW EVOLUTION MONITORING FOR AIRCRAFT ICING STUDY
Abstract. Monitoring the evolution of the aerodynamic flow in potentially dangerous conditions is very important to ensure flight safety. Due to the impossibility of experimental study of critical flight conditions in real flights, methods of scaled modeling of flow processes have been developed and are widely used in aerodynamics and hydrodynamics. Aircraft icing is one of the most important processes that pose a threat to flight safety. The presented study is aimed at developing techniques for monitoring of process of aircraft icing and its influence on flow behaviour, that can be used in controlled conditions of aerodynamic/hydrodynamic tube. While available technical means for aerodynamic study does not include the wind tunnel for registration of flow simultaneously with icing process, the proposed framework includes as icing process 3D registration so further modelling this process in a hydrodynamic tube for flow monitoring. The proposed technique includes three phases, that allow to perform comprehensive monitoring of the whole process beginning with 3D registration of ice accretion development and completing with accurate 3D flow evolution monitoring corresponding to icing process.
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
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Online-Ressource
- Language
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Englisch
- Bibliographic citation
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FLOW EVOLUTION MONITORING FOR AIRCRAFT ICING STUDY ; volume:XLVIII-2/W3-2023 ; year:2023 ; pages:129-135 ; extent:7
The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences ; XLVIII-2/W3-2023 (2023), 129-135 (gesamt 7)
- Creator
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Knyaz, V. A.
Kniaz, V. V.
Ippolitov, E. V.
Novikov, M. M.
Zheltov, S. Y.
- DOI
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10.5194/isprs-archives-XLVIII-2-W3-2023-129-2023
- URN
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urn:nbn:de:101:1-2023051804333579289070
- Rights
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Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
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14.08.2025, 10:44 AM CEST
Data provider
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Knyaz, V. A.
- Kniaz, V. V.
- Ippolitov, E. V.
- Novikov, M. M.
- Zheltov, S. Y.
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Health Monitoring for Aircraft Systems using Decision Trees and Genetic Evolution
3D RECONSTRUCTION OF ICE SHAPE USING VISIBLE AND THERMAL RANGE IMAGING FOR AIRCRAFT ICING STUDY
Geometric characterization of aircraft icing
Aircraft de-icing occurence prediciton
Aircraft icing : a challenging problem of fluid mechanics.
ADWICE: Advanced diagnosis and warning system for aircraft icing environments
Experimental and numerical studies on ice crystal icing of civil aircraft
Multiphysical and multi scale modelling of composite materials for aircraft De-Icing
A new parameterization of aircraft icing accounting for microphysical properties of clouds
Composite Materials For Creation Of Anti-Icing Elements And Other Aircraft Systems
Fixed-time angle of attack constrained control for aircraft considering dynamic icing process
Micro/nano manufacturing aircraft surface with anti-icing and deicing performances: An overview
Health Monitoring for Aircraft Systems using Decision Trees and Genetic Evolution
3D RECONSTRUCTION OF ICE SHAPE USING VISIBLE AND THERMAL RANGE IMAGING FOR AIRCRAFT ICING STUDY
Geometric characterization of aircraft icing
Aircraft de-icing occurence prediciton
Aircraft icing : a challenging problem of fluid mechanics.
ADWICE: Advanced diagnosis and warning system for aircraft icing environments
Experimental and numerical studies on ice crystal icing of civil aircraft
Multiphysical and multi scale modelling of composite materials for aircraft De-Icing
A new parameterization of aircraft icing accounting for microphysical properties of clouds
Composite Materials For Creation Of Anti-Icing Elements And Other Aircraft Systems
Fixed-time angle of attack constrained control for aircraft considering dynamic icing process
Micro/nano manufacturing aircraft surface with anti-icing and deicing performances: An overview
Health Monitoring for Aircraft Systems using Decision Trees and Genetic Evolution