Littérature scientifique sur le sujet « Hypersonic Transportation Systems »
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Articles de revues sur le sujet "Hypersonic Transportation Systems"
Viola, Nicole, Roberta Fusaro et Valeria Vercella. « Technology roadmapping methodology for future hypersonic transportation systems ». Acta Astronautica 195 (juin 2022) : 430–44. http://dx.doi.org/10.1016/j.actaastro.2022.03.038.
Texte intégralViola, Nicole, Pietro Roncioni, Oscar Gori et Roberta Fusaro. « Aerodynamic Characterization of Hypersonic Transportation Systems and Its Impact on Mission Analysis ». Energies 14, no 12 (16 juin 2021) : 3580. http://dx.doi.org/10.3390/en14123580.
Texte intégralFusaro, Roberta, Valeria Vercella, Davide Ferretto, Nicole Viola et Johan Steelant. « Economic and environmental sustainability of liquid hydrogen fuel for hypersonic transportation systems ». CEAS Space Journal 12, no 3 (18 avril 2020) : 441–62. http://dx.doi.org/10.1007/s12567-020-00311-x.
Texte intégralVeeran, Sasha, Apostolos Pesyridis et Lionel Ganippa. « Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine ». Energies 11, no 10 (25 septembre 2018) : 2558. http://dx.doi.org/10.3390/en11102558.
Texte intégralFusaro, Roberta, et Nicole Viola. « Preliminary reliability and safety assessment methodology for trans-atmospheric transportation systems ». Aircraft Engineering and Aerospace Technology 90, no 4 (8 mai 2018) : 639–51. http://dx.doi.org/10.1108/aeat-11-2016-0214.
Texte intégralD’Oriano, Vera, Raffaele Savino et Michele Visone. « Aerothermodynamic study of a small hypersonic plane ». Aircraft Engineering and Aerospace Technology 90, no 2 (5 mars 2018) : 471–80. http://dx.doi.org/10.1108/aeat-06-2015-0151.
Texte intégralCresto Aleina, Sara, Nicole Viola, Roberta Fusaro, José Longo et Giorgio Saccoccia. « Basis for a methodology for roadmaps generation for hypersonic and re-entry space transportation systems ». Technological Forecasting and Social Change 128 (mars 2018) : 208–25. http://dx.doi.org/10.1016/j.techfore.2017.12.004.
Texte intégralFerretto, Davide, Roberta Fusaro et Nicole Viola. « Innovative Multiple Matching Charts approach to support the conceptual design of hypersonic vehicles ». Proceedings of the Institution of Mechanical Engineers, Part G : Journal of Aerospace Engineering 234, no 12 (24 avril 2020) : 1893–912. http://dx.doi.org/10.1177/0954410020920037.
Texte intégralViola, Nicole, Roberta Fusaro, Valeria Vercella et Giorgio Saccoccia. « Technology RoadmappIng Strategy, TRIS : Methodology and tool for technology roadmaps for hypersonic and re-entry space transportation systems ». Acta Astronautica 170 (mai 2020) : 609–22. http://dx.doi.org/10.1016/j.actaastro.2020.01.037.
Texte intégralBandivadekar, Deep, et Edmondo Minisci. « Modelling and Simulation of Transpiration Cooling Systems for Atmospheric Re-Entry ». Aerospace 7, no 7 (1 juillet 2020) : 89. http://dx.doi.org/10.3390/aerospace7070089.
Texte intégralThèses sur le sujet "Hypersonic Transportation Systems"
FERRETTO, DAVIDE. « Innovative Model Based Systems Engineering approach for the design of hypersonic transportation systems ». Doctoral thesis, Politecnico di Torino, 2020. http://hdl.handle.net/11583/2839867.
Texte intégralSziroczak, David. « Conceptual design methodologies appropriate to hypersonic space and global transportation systems ». Thesis, Cranfield University, 2015. http://dspace.lib.cranfield.ac.uk/handle/1826/9885.
Texte intégralCRESTO, ALEINA SARA. « Design methodologies for space systems in a System of Systems (SoS) architecture ». Doctoral thesis, Politecnico di Torino, 2020. http://hdl.handle.net/11583/2790162.
Texte intégralFUSARO, ROBERTA. « Comparative analysis of new configurations of aircraft aimed at competitiveness, environmental compatibility and safety ». Doctoral thesis, Politecnico di Torino, 2017. http://hdl.handle.net/11583/2694988.
Texte intégralΠαναγιωτόπουλος, Ηλίας. « Ροές υψηλών ταχυτήτων και θερμοδυναμική αερίων σε υψηλές θερμοκρασίες : υπολογιστική διερεύνηση της εισόδου και επαναφοράς υπερυπερηχητικών συστημάτων μεταφοράς στην ατμόσφαιρα ». Thesis, 2008. http://nemertes.lis.upatras.gr/jspui/handle/10889/1540.
Texte intégralThe object of the present doctoral thesis constitutes the theoretical and calculating simulation of high-speed atmospheric flightmotion, with particular emphasis in hypersonic speeds and aerodynamic and thermodynamic analysis. The methodology that is followed has as main aim the prediction of return flight trace of hypersonic vehicles in Earth’s ground, assuming the speeds of flight to reach the 15000 m/s (Mach number ~ 40) and stagnation temperatures the 15000 K. In this work are followed methodological approach and systematic bibliographic research in the scientific field of aerodynamic overheating that suffers Hypersonic Vehicles(H/V) at their flight in Earth’s atmosphere. The analysis of hypersonic flow, thermal loads and new methods for thermal protection systems of H/V are developed the last decades and are evolved continuously, but until today (2008) resulting failures mainly at their reentry in atmosphere from the interval. For the simulation of the atmospheric hypersonic flight motion become study and analysis of thermodynamic properties and parameters, that characterize the flow fields in high speeds and high temperatures. The determination of altered flow conditions, thermodynamic properties and transport magnitudes will contribute in the theories of modelling and high thermal strain calculations, in the constitution of overheating air and it’s high temperature determination in the external surface of heat insulation wall of high-speed vehicles at their flight in Earth’s atmosphere. In this work are developed calculating algorithms of simulation for the successful prediction of atmospheric flight motion of hypersonic transport vehicles. The basic aerodynamic characteristics of lifting vehicles in high speeds are calculated with suitable adaptation of classic Newtonian Flow in high speeds and are confirmed with experimental data of aerodynamic measurements in high speed wind-tunnels of NASA. Moreover in this thesis are incorporated models for the simulation of properties of overheating air behaviour as real gas in thermodynamic balance in extreme flow conditions (high speeds, high pressures and low densities). Particularly becomes analysis of the altered constitution and properties of air (thermodynamic magnitudes and transport magnitudes) in very high temperatures on hypersonic flow field. This study will lead to the export of a new model for the transported thermal stagnation region calculations of hypersonic vehicles, which is confirmed so much with internationally recognized thermal models (as that of Fay-Riddell) and with calculating simulations of other researchers. The methodology that is followed will constitute the base for the export of a new theoretical model for high temperature air calculations in thermal protection systems surface of hypersonic vehicles. The effectiveness of proposed methodology, with the combination kinematic and aerothermodynamics analysis in united calculating algorithm, is proved and confirmed via the application of above simulation models on ballistic (Apollo Command Module) and lifting (Space Transportation System, known as Space Shuttle) hypersonic vehicles. The results of proposed method are compared, evaluated and certified with similarly by internationally recognized calculating systems and experimental data of measurements in hypersonic wind-tunnels for high speed vehicles. In the next decades, the development of hypersonic transportation systems will be rapid and particularly attractive from technological side with hopeful messages for “earthy” transfers with high speeds in short times, but also likely persons-astronaut missions in other planets of solar system. Thus the present doctoral thesis, developing the progress that has taken place in the past few years, is appreciated that it contributes substantially in still under development - for the Greek data unusual - scientific field of Hypersonic Aerothermodynamics, and in the growth of methodology for the aerothermodynamic construction of hypersonic vehicles. The proposed complex model of kinematic and thermodynamic calculating analysis and it’s methodology that is followed have influence and application in the majority of cases of hypersonic flights in earthy and, with properly adaptations, in anyone planetary atmosphere. Of course, the proposed methodology has margins of development and growth in order to improve her efficiency with the import of also new elements and also extended the spectrum of her possible applications.
Chapitres de livres sur le sujet "Hypersonic Transportation Systems"
Griebel, Hannes. « Transportation and Deployment System ». Dans Reaching High Altitudes on Mars with an Inflatable Hypersonic Drag Balloon (Ballute), 155–68. Wiesbaden : Vieweg+Teubner, 2011. http://dx.doi.org/10.1007/978-3-8348-9911-8_8.
Texte intégralActes de conférences sur le sujet "Hypersonic Transportation Systems"
Hueter, Uwe. « Advanced Reusable Transportation Technologies Project overview ». Dans Space Plane and Hypersonic Systems and Technology Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-4603.
Texte intégralPuettmann, Norbert. « Tetra - Technologies for reusable future space transportation systems ». Dans 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4927.
Texte intégralDecker, Klaus. « Aerodynamic coefficients for realistic space transportation systems in lateral motion ». Dans 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4805.
Texte intégralKostromin, S., A. Romashkin et G. Efanova. « Study on validation of the design principles of the 'Oryol' Space Transportation System ». Dans Space Plane and Hypersonic Systems and Technology Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-4491.
Texte intégralFujii, Kenji, et Shinji Ishimoto. « Research Activities to Realize Advanced Space Transportation System ». Dans 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-2575.
Texte intégralSchroeder, W., R. Behr et S. Menne. « Analysis of hypersonic flows around space transportation systems via CFD methods ». Dans 5th International Aerospace Planes and Hypersonics Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-5067.
Texte intégralAngelini, Roberto, Luciano Basile, Massimiliano Bottacini, Federico Massobrio, Marco Caporicci, Rafael Molina et Ulrich Thomas. « Study on Human Space Transportation Systems and Re-Entry Demonstrators ». Dans 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-7936.
Texte intégralGrallert, H., et H. Kuczera. « Kick-stages - A mandatory element of future reusable space transportation systems ». Dans 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4885.
Texte intégralGrallert, H. « Synthesis of a FESTIP air-breathing TSTO space transportation system ». Dans 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-4884.
Texte intégralEngler, V., D. Coors et D. Jacob. « Optimization of a space transportation system including design sensitivities ». Dans 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-1553.
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