Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft

In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagne...
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Autor*in:	Cheng Liangliang [verfasserIn] Yue Kuizhi [verfasserIn] Guo Weigang [verfasserIn] Yu Dazhao [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2016

Schlagwörter:	Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation

Übergeordnetes Werk:	In: Journal of Aerospace Technology and Management - Instituto de Aeronáutica e Espaço (IAE), 2010, 8(2016), 1
Übergeordnetes Werk:	volume:8 ; year:2016 ; number:1

Links:	Link aufrufen Link aufrufen Journal toc

Katalog-ID:	DOAJ024522023

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520			\|a In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts.
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allfields	(DE-627)DOAJ024522023 (DE-599)DOAJ2f1e42eced184542aefb56135dca4d53 DE-627 ger DE-627 rakwb eng TL1-4050 Cheng Liangliang verfasserin aut Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts. Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation Technology T Motor vehicles. Aeronautics. Astronautics Yue Kuizhi verfasserin aut Guo Weigang verfasserin aut Yu Dazhao verfasserin aut In Journal of Aerospace Technology and Management Instituto de Aeronáutica e Espaço (IAE), 2010 8(2016), 1 (DE-627)633082236 (DE-600)2567333-6 21759146 nnns volume:8 year:2016 number:1 https://doaj.org/article/2f1e42eced184542aefb56135dca4d53 kostenfrei https://www.jatm.com.br/jatm/article/view/514 kostenfrei https://doaj.org/toc/2175-9146 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2016 1
spelling	(DE-627)DOAJ024522023 (DE-599)DOAJ2f1e42eced184542aefb56135dca4d53 DE-627 ger DE-627 rakwb eng TL1-4050 Cheng Liangliang verfasserin aut Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts. Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation Technology T Motor vehicles. Aeronautics. Astronautics Yue Kuizhi verfasserin aut Guo Weigang verfasserin aut Yu Dazhao verfasserin aut In Journal of Aerospace Technology and Management Instituto de Aeronáutica e Espaço (IAE), 2010 8(2016), 1 (DE-627)633082236 (DE-600)2567333-6 21759146 nnns volume:8 year:2016 number:1 https://doaj.org/article/2f1e42eced184542aefb56135dca4d53 kostenfrei https://www.jatm.com.br/jatm/article/view/514 kostenfrei https://doaj.org/toc/2175-9146 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2016 1
allfields_unstemmed	(DE-627)DOAJ024522023 (DE-599)DOAJ2f1e42eced184542aefb56135dca4d53 DE-627 ger DE-627 rakwb eng TL1-4050 Cheng Liangliang verfasserin aut Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts. Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation Technology T Motor vehicles. Aeronautics. Astronautics Yue Kuizhi verfasserin aut Guo Weigang verfasserin aut Yu Dazhao verfasserin aut In Journal of Aerospace Technology and Management Instituto de Aeronáutica e Espaço (IAE), 2010 8(2016), 1 (DE-627)633082236 (DE-600)2567333-6 21759146 nnns volume:8 year:2016 number:1 https://doaj.org/article/2f1e42eced184542aefb56135dca4d53 kostenfrei https://www.jatm.com.br/jatm/article/view/514 kostenfrei https://doaj.org/toc/2175-9146 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2016 1
allfieldsGer	(DE-627)DOAJ024522023 (DE-599)DOAJ2f1e42eced184542aefb56135dca4d53 DE-627 ger DE-627 rakwb eng TL1-4050 Cheng Liangliang verfasserin aut Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts. Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation Technology T Motor vehicles. Aeronautics. Astronautics Yue Kuizhi verfasserin aut Guo Weigang verfasserin aut Yu Dazhao verfasserin aut In Journal of Aerospace Technology and Management Instituto de Aeronáutica e Espaço (IAE), 2010 8(2016), 1 (DE-627)633082236 (DE-600)2567333-6 21759146 nnns volume:8 year:2016 number:1 https://doaj.org/article/2f1e42eced184542aefb56135dca4d53 kostenfrei https://www.jatm.com.br/jatm/article/view/514 kostenfrei https://doaj.org/toc/2175-9146 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2016 1
allfieldsSound	(DE-627)DOAJ024522023 (DE-599)DOAJ2f1e42eced184542aefb56135dca4d53 DE-627 ger DE-627 rakwb eng TL1-4050 Cheng Liangliang verfasserin aut Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts. Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation Technology T Motor vehicles. Aeronautics. Astronautics Yue Kuizhi verfasserin aut Guo Weigang verfasserin aut Yu Dazhao verfasserin aut In Journal of Aerospace Technology and Management Instituto de Aeronáutica e Espaço (IAE), 2010 8(2016), 1 (DE-627)633082236 (DE-600)2567333-6 21759146 nnns volume:8 year:2016 number:1 https://doaj.org/article/2f1e42eced184542aefb56135dca4d53 kostenfrei https://www.jatm.com.br/jatm/article/view/514 kostenfrei https://doaj.org/toc/2175-9146 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2016 1
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callnumber-first	T - Technology
author	Cheng Liangliang
spellingShingle	Cheng Liangliang misc TL1-4050 misc Conceptual design misc Stealth misc Strike fighter misc Computational Fluid Dynamics misc Simulation misc Technology misc T misc Motor vehicles. Aeronautics. Astronautics Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft
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topic_title	TL1-4050 Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft Conceptual design Stealth Strike fighter Computational Fluid Dynamics Simulation
topic	misc TL1-4050 misc Conceptual design misc Stealth misc Strike fighter misc Computational Fluid Dynamics misc Simulation misc Technology misc T misc Motor vehicles. Aeronautics. Astronautics
topic_unstemmed	misc TL1-4050 misc Conceptual design misc Stealth misc Strike fighter misc Computational Fluid Dynamics misc Simulation misc Technology misc T misc Motor vehicles. Aeronautics. Astronautics
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title	Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft
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title_full	Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft
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author_browse	Cheng Liangliang Yue Kuizhi Guo Weigang Yu Dazhao
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author-letter	Cheng Liangliang
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title_sort	integration analysis of conceptual design and stealth-aerodynamic characteristics of combat aircraft
callnumber	TL1-4050
title_auth	Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft
abstract	In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts.
abstractGer	In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts.
abstract_unstemmed	In order to study stealth strike-fighter, an analysis on stealth-aerodynamic integration and conceptual design is conducted. A conceptual 3-D digital model with internal antiship missiles and air-to-air missiles is designed in CATIA software. Based on the physical optics and equivalent electromagnetic current methods, using the self-programmed RCSAnsys software, the Radar Cross Section (RCS) characteristics and characteristics of scattering intensity distribution of the model are numerically simulated. Based on the turbulence theory of standard k-ε equations, using Fluent software, the pressure, velocity and lift-to-drag characteristics of the conceptual aircraft are numerically simulated. The simulation results show that the stealth and aerodynamic characteristics of the conceptual aircraft can be designed through integration analysis process, which can provide technical support to the design of the advanced operational aircrafts.
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title_short	Integration Analysis of Conceptual Design and Stealth-Aerodynamic Characteristics of Combat Aircraft
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up_date	2024-07-03T23:18:53.899Z
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