In order to design the thermal control system of a spacecraft (satellite, space probe or manned vehicle), thermal engineer uses dedicated software. As the radiative component may play a predominant role, a ray tracing algorithm is used to compute view factors and radiative exchanges between surfaces of finite dimensions, assumed isothermal. External flows are also evaluated by ray tracing while the conductive couplings are usually encoded manually by the user. As ray tracing is based on a random process, the achieved accuracy is determined by the number of traced rays. In general, the choice of the number of rays is left at the discretion of the engineer, which can lead to errors. Another disadvantage of ray tracing is its low convergence. An acceleration method of ray tracing is necessary. An order of magnitude improvement in performance over existing Monte Carlo ray tracing techniques used for space thermal analysis, a statistical accuracy control to lead the thermal engineer during ray tracing, a simple approach combining conduction and radiation, geometry and finite elements, these are parts of the objectives reached in this thesis.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
After studying engineering at National School of Aeronautics and Space (Supaero), Pierre Vueghs obtained a degree in Physical Engineering at the University of Liège. Research fellow at the Belgian Fund for Scientific Research, he performed a thesis with European Space Agency on thermal analysis. Now, he works as Doctor Engineer at LMS-Samtech.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In order to design the thermal control system of a spacecraft (satellite, space probe or manned vehicle), thermal engineer uses dedicated software. As the radiative component may play a predominant role, a ray tracing algorithm is used to compute view factors and radiative exchanges between surfaces of finite dimensions, assumed isothermal. External flows are also evaluated by ray tracing while the conductive couplings are usually encoded manually by the user. As ray tracing is based on a random process, the achieved accuracy is determined by the number of traced rays. In general, the choice of the number of rays is left at the discretion of the engineer, which can lead to errors. Another disadvantage of ray tracing is its low convergence. An acceleration method of ray tracing is necessary. An order of magnitude improvement in performance over existing Monte Carlo ray tracing techniques used for space thermal analysis, a statistical accuracy control to lead the thermal engineer during ray tracing, a simple approach combining conduction and radiation, geometry and finite elements, these are parts of the objectives reached in this thesis. 284 pp. Englisch. N° de réf. du vendeur 9783659115806
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Taschenbuch. Etat : Neu. Innovative Ray Tracing Algorithms for Space Thermal Analysis | From rendering to space thermal applications | Pierre Vueghs | Taschenbuch | 284 S. | Englisch | 2016 | LAP LAMBERT Academic Publishing | EAN 9783659115806 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 106470104
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -In order to design the thermal control system of a spacecraft (satellite, space probe or manned vehicle), thermal engineer uses dedicated software. As the radiative component may play a predominant role, a ray tracing algorithm is used to compute view factors and radiative exchanges between surfaces of finite dimensions, assumed isothermal. External flows are also evaluated by ray tracing while the conductive couplings are usually encoded manually by the user. As ray tracing is based on a random process, the achieved accuracy is determined by the number of traced rays. In general, the choice of the number of rays is left at the discretion of the engineer, which can lead to errors. Another disadvantage of ray tracing is its low convergence. An acceleration method of ray tracing is necessary. An order of magnitude improvement in performance over existing Monte Carlo ray tracing techniques used for space thermal analysis, a statistical accuracy control to lead the thermal engineer during ray tracing, a simple approach combining conduction and radiation, geometry and finite elements, these are parts of the objectives reached in this thesis.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 284 pp. Englisch. N° de réf. du vendeur 9783659115806
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In order to design the thermal control system of a spacecraft (satellite, space probe or manned vehicle), thermal engineer uses dedicated software. As the radiative component may play a predominant role, a ray tracing algorithm is used to compute view factors and radiative exchanges between surfaces of finite dimensions, assumed isothermal. External flows are also evaluated by ray tracing while the conductive couplings are usually encoded manually by the user. As ray tracing is based on a random process, the achieved accuracy is determined by the number of traced rays. In general, the choice of the number of rays is left at the discretion of the engineer, which can lead to errors. Another disadvantage of ray tracing is its low convergence. An acceleration method of ray tracing is necessary. An order of magnitude improvement in performance over existing Monte Carlo ray tracing techniques used for space thermal analysis, a statistical accuracy control to lead the thermal engineer during ray tracing, a simple approach combining conduction and radiation, geometry and finite elements, these are parts of the objectives reached in this thesis. N° de réf. du vendeur 9783659115806
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