Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method

Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated and meshed with th...
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Autor*in:	Wei Gao [verfasserIn] Yishu Liu [verfasserIn] Qifu Li [verfasserIn] Bei Lu [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2023

Schlagwörter:	unsteady vortex lattice method multi-lifting surfaces aerodynamic modeling

Übergeordnetes Werk:	In: Aerospace - MDPI AG, 2014, 10(2023), 2, p 203
Übergeordnetes Werk:	volume:10 ; year:2023 ; number:2, p 203

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc

DOI / URN:	10.3390/aerospace10020203

Katalog-ID:	DOAJ081038453

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520			\|a Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated and meshed with the object-oriented data structure. The physical influence between different lifting surfaces was modeled, and the wake–surface interaction was also considered by using different built-in vortex core models. The trajectory data were used to replace the pre-calculated downwash superposition for boundary condition integration, and the instantaneous boundary condition was generated directly from the kinematic states and mesh messages of the model concerned. Considering the direct coupling effect between aerodynamics and rigid body dynamics, the function for free flight was built for medium-fidelity dynamic simulations and aerodynamic data identifications. The proposed high-efficiency modeling and simulation process can be easily applied to models with any number of different lifting surfaces and arbitrary motion modes.
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language	English
source	In Aerospace 10(2023), 2, p 203 volume:10 year:2023 number:2, p 203
sourceStr	In Aerospace 10(2023), 2, p 203 volume:10 year:2023 number:2, p 203
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	unsteady vortex lattice method multi-lifting surfaces aerodynamic modeling Motor vehicles. Aeronautics. Astronautics
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container_title	Aerospace
authorswithroles_txt_mv	Wei Gao @@aut@@ Yishu Liu @@aut@@ Qifu Li @@aut@@ Bei Lu @@aut@@
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callnumber-first	T - Technology
author	Wei Gao
spellingShingle	Wei Gao misc TL1-4050 misc unsteady vortex lattice method misc multi-lifting surfaces misc aerodynamic modeling misc Motor vehicles. Aeronautics. Astronautics Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method
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topic_title	TL1-4050 Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method unsteady vortex lattice method multi-lifting surfaces aerodynamic modeling
topic	misc TL1-4050 misc unsteady vortex lattice method misc multi-lifting surfaces misc aerodynamic modeling misc Motor vehicles. Aeronautics. Astronautics
topic_unstemmed	misc TL1-4050 misc unsteady vortex lattice method misc multi-lifting surfaces misc aerodynamic modeling misc Motor vehicles. Aeronautics. Astronautics
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title	Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method
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title_full	Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method
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title_sort	aerodynamic modeling and simulation of multi-lifting surfaces based on the unsteady vortex lattice method
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title_auth	Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method
abstract	Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated and meshed with the object-oriented data structure. The physical influence between different lifting surfaces was modeled, and the wake–surface interaction was also considered by using different built-in vortex core models. The trajectory data were used to replace the pre-calculated downwash superposition for boundary condition integration, and the instantaneous boundary condition was generated directly from the kinematic states and mesh messages of the model concerned. Considering the direct coupling effect between aerodynamics and rigid body dynamics, the function for free flight was built for medium-fidelity dynamic simulations and aerodynamic data identifications. The proposed high-efficiency modeling and simulation process can be easily applied to models with any number of different lifting surfaces and arbitrary motion modes.
abstractGer	Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated and meshed with the object-oriented data structure. The physical influence between different lifting surfaces was modeled, and the wake–surface interaction was also considered by using different built-in vortex core models. The trajectory data were used to replace the pre-calculated downwash superposition for boundary condition integration, and the instantaneous boundary condition was generated directly from the kinematic states and mesh messages of the model concerned. Considering the direct coupling effect between aerodynamics and rigid body dynamics, the function for free flight was built for medium-fidelity dynamic simulations and aerodynamic data identifications. The proposed high-efficiency modeling and simulation process can be easily applied to models with any number of different lifting surfaces and arbitrary motion modes.
abstract_unstemmed	Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated and meshed with the object-oriented data structure. The physical influence between different lifting surfaces was modeled, and the wake–surface interaction was also considered by using different built-in vortex core models. The trajectory data were used to replace the pre-calculated downwash superposition for boundary condition integration, and the instantaneous boundary condition was generated directly from the kinematic states and mesh messages of the model concerned. Considering the direct coupling effect between aerodynamics and rigid body dynamics, the function for free flight was built for medium-fidelity dynamic simulations and aerodynamic data identifications. The proposed high-efficiency modeling and simulation process can be easily applied to models with any number of different lifting surfaces and arbitrary motion modes.
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title_short	Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method
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Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method

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