Littérature scientifique sur le sujet « Hypersonic aircraft design »
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Articles de revues sur le sujet "Hypersonic aircraft design"
Alkaya, Can, Ashish Alex Sam et Apostolos Pesyridis. « Conceptual Advanced Transport Aircraft Design Configuration for Sustained Hypersonic Flight ». Aerospace 5, no 3 (1 septembre 2018) : 91. http://dx.doi.org/10.3390/aerospace5030091.
Texte intégralDai, Yalin, Yu Wang, Xiaoyu Xu et Xiongqing Yu. « An Improved Method for Initial Sizing of Airbreathing Hypersonic Aircraft ». Aerospace 10, no 2 (18 février 2023) : 199. http://dx.doi.org/10.3390/aerospace10020199.
Texte intégralKoptev, A. « "THEORETICAL ASPECTS OF STRENGTH AND THERMAL CONTROL OF HYPERSONIC AIRCRAFT" ». National Association of Scientists 1, no 66 (14 mai 2021) : 54–60. http://dx.doi.org/10.31618/nas.2413-5291.2021.1.66.403.
Texte intégralChen, Jie, Yan Lin et Chang Peng Pan. « Hypersonic Aircraft Nonlinear Fault-Tolerant Controller Design ». Applied Mechanics and Materials 494-495 (février 2014) : 1056–59. http://dx.doi.org/10.4028/www.scientific.net/amm.494-495.1056.
Texte intégralMorrell, Benjamin J., David J. Munk, Gareth A. Vio et Dries Verstraete. « Development of a Hypersonic Aircraft Design Optimization Tool ». Applied Mechanics and Materials 553 (mai 2014) : 847–52. http://dx.doi.org/10.4028/www.scientific.net/amm.553.847.
Texte intégralWang, Zhiqiang, Anjing Zhang, Jia Pan, Weiguo Lu et Yubiao Sun. « Fluid-Thermal Interaction Simulation of a Hypersonic Aircraft Optical Dome ». Energies 15, no 22 (17 novembre 2022) : 8619. http://dx.doi.org/10.3390/en15228619.
Texte intégralYang, Jie, Song Ping Wu et Wen Xin Hou. « A Method for Aerodynamic Characteristic Analysis of Hypersonic Aircraft Based on Response Surface Model ». Applied Mechanics and Materials 477-478 (décembre 2013) : 277–80. http://dx.doi.org/10.4028/www.scientific.net/amm.477-478.277.
Texte intégralWang, Yuhui, Peng Shao, Qingxian Wu et Mou Chen. « Reliability analysis for a hypersonic aircraft’s wing spar ». Aircraft Engineering and Aerospace Technology 91, no 4 (1 avril 2019) : 549–57. http://dx.doi.org/10.1108/aeat-11-2017-0242.
Texte intégralCastigliola, Luca, Flavia Causa et Michele Grassi. « Navigation architecture for hypersonic aircraft ». MATEC Web of Conferences 304 (2019) : 04008. http://dx.doi.org/10.1051/matecconf/201930404008.
Texte intégralJiao, Xin, et Ju Jiang. « Design of adaptive switching control for hypersonic aircraft ». Advances in Mechanical Engineering 7, no 10 (21 octobre 2015) : 168781401561046. http://dx.doi.org/10.1177/1687814015610465.
Texte intégralThèses sur le sujet "Hypersonic aircraft design"
Javiad, Kashif Hussan. « Development of conceptual and preliminary design methodologies for hypersonic military aircraft ». Thesis, Imperial College London, 2005. http://hdl.handle.net/10044/1/7150.
Texte intégralFiorentini, Lisa. « Nonlinear Adaptive Controller Design For Air-breathing Hypersonic Vehicles ». The Ohio State University, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=osu1274986563.
Texte intégralDicara, Daniel L. « Development of an aerodynamic/RCS framework for the preliminary design of a hypersonic aircraft ». Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/46570.
Texte intégralIncludes bibliographical references (p. 59-60).
The design of hypersonic airbreathing aircraft pushes the envelope of current state-ofthe-art aerospace propulsion and materials technology. Therefore, these aircraft are highly integrated to produce adequate thrust, reduce drag, and limit surface heating. Consequently, every aircraft component (e.g., wings, fuselage, propulsion system) is sensitive to changes in every other component. Including Radar Cross Section (RCS) considerations further complicates matters. During preliminary design, this requires the rapid analysis of different aircraft configurations to investigate component interactions and determine performance trends. This thesis presents a framework and accompanying software for performing such an analysis. The intent is to optimize a hypersonic airbreathing aircraft design in terms of aerodynamic performance and RCS. Computational Fluid Dynamics (CFD) and Computational Electromagnetics (CEM) are the two main framework software components. CFD simulates airflow around the aircraft to analyze its aerodynamic performance. Alternately, CEM simulates the electromagnetic signature of the aircraft to predict its RCS. The framework begins with the generation of a three-dimensional computer aided design aircraft model. Next, a grid generator discretizes this model. The flow simulation is performed on this grid and the aircraft's aerodynamic characteristics are determined. Flow visualization aids this determination. Then, aircraft geometry refinements are made to improve aerodynamic performance. Afterward, CEM is performed on aerodynamically favorable designs at various aspect angles and frequencies. RCS values are determined and used to rank the different configurations. Also, inverse synthetic aperture radar images are generated to locate major scattering centers and aid the design refinement. The design loop continues in this fashion until an acceptable aircraft design is achieved. The NASA X-43A test vehicle was used to validate this preliminary design framework.
by Daniel L. DiCara.
S.M.
Sharifzadeh, Shayan. « Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles ». Thesis, The University of Sydney, 2017. http://hdl.handle.net/2123/19127.
Texte intégralSharifzadeh, Shayan. « Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles ». Doctoral thesis, Universite Libre de Bruxelles, 2017. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/255764.
Texte intégralDoctorat en Sciences de l'ingénieur et technologie
This thesis was conducted in co-tutelle between University of Sydney and Université Libre de Bruxelles.Professor Dries Verstraete was my supervisor at the University of Sydney (so as a member of SydneyUni), but is automatically registered here as a member of ULB because he worked at ULB almost ten years ago.Ben Thornber is also a member of the University of Sydney but the application does not save it for an unknown reason.
info:eu-repo/semantics/nonPublished
Chalker, Jack Randolph. « Design and Manipulation of a Power-Generating System with High-Temperature Fuel Cells for Hypersonic Applications ». Wright State University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1567169603256774.
Texte intégralTancred, James Anderson. « Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging ». University of Dayton / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543801033672049.
Texte intégralLivres sur le sujet "Hypersonic aircraft design"
Hani, Alkamhawi, et United States. National Aeronautics and Space Administration., dir. Hypersonic aircraft design. [Columbus, Ohio] : Ohio State University, 1990.
Trouver le texte intégralArdema, Mark D. Body weight of hypersonic aircraft. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1988.
Trouver le texte intégralA, Mackley Ernest, et Langley Research Center, dir. NASA's hypersonic research engine project : A review. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1994.
Trouver le texte intégralJ, Chattot J., Lawrence S. L et United States. National Aeronautics and Space Administration., dir. Parallelization of a parabolized Navier-Stokes solver with a design optimizer : 34th AIAA Aerospace Sciences Meeting and Exhibit. [Washington, DC : National Aeronautics and Space Administration, 1996.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Trouver le texte intégralGatlin, Gregory M. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. Hampton, Va : Langley Research Center, 1989.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Aeropropulsion '91 : Proceedings of a conference held at NASA Lewis Research Center, Cleveland, Ohio, March 20-21, 1991. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Trouver le texte intégralAdvanced hypersonic aircraft design. [Columbus, Ohio] : Ohio State University, Aeronautical and Astronautical Engineering, 1992.
Trouver le texte intégralAeropropulsion '91 : Proceedings of a conference held at NASA Lewis Research Center, Cleveland, Ohio, March 20-21, 1991. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Trouver le texte intégralChapitres de livres sur le sujet "Hypersonic aircraft design"
Merlen, A. « From the analytical theory to hypersonic aircraft design ». Dans Asymptotic Modelling in Fluid Mechanics, 221–28. Berlin, Heidelberg : Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/3-540-59414-0_69.
Texte intégralYang, Zhiling, et Hongfei Sun. « Nonlinear Control Design of a Hypersonic Aircraft Using Sum-of-Squares Method ». Dans Informatics in Control, Automation and Robotics, 333–42. Berlin, Heidelberg : Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-25992-0_48.
Texte intégralMartin, Katharina, Dennis Daub, Burkard Esser, Ali Gülhan et Stefanie Reese. « Numerical Modelling of Fluid-Structure Interaction for Thermal Buckling in Hypersonic Flow ». Dans Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 341–55. Cham : Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_22.
Texte intégralKossira, H., A. Bardenhagen et W. Heinze. « An Integrated Computer-Program-System for the Preliminary Design of Advanced Hypersonic Aircraft (PrADO-Hy) ». Dans Orbital Transport, 129–47. Berlin, Heidelberg : Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-45720-3_9.
Texte intégralGuo, Yixiang, Lifang Chen et Yuhang Zhou. « A Review of the Development of Sealing Materials and Measurement and Control Simulation Technology for Typical Hypersonic Vehicle Positions ». Dans Proceedings of the 2022 International Conference on Smart Manufacturing and Material Processing (SMMP2022). IOS Press, 2022. http://dx.doi.org/10.3233/atde220826.
Texte intégralActes de conférences sur le sujet "Hypersonic aircraft design"
JOHNSON, REUBEN. « Soviet applications for hypersonic vehicles ». Dans Aircraft Design, Systems and Operations Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4507.
Texte intégralCOONS, L. « Propulsion challenges for hypersonic flight ». Dans Aircraft Systems, Design and Technology Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2620.
Texte intégralTRIKHA, ARUN, et THOMAS CREIGHTON. « Crew escape system design for hypersonic vehicles ». Dans Aircraft Design and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2025.
Texte intégralARDEMA, MARK, ERIC TERJESEN et CATHY ROBERTS. « Body weight of advanced concept hypersonic aircraft ». Dans Aircraft Design and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3180.
Texte intégralWARD, RICHARD, MARK LEAGUE et EDDIE MOORE. « Assessment of a Soviet hypersonic transport ». Dans Aircraft Design, Systems and Operations Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4506.
Texte intégralCHAPUT, ARMAND. « Preliminary sizing methodology for hypersonic vehicles ». Dans Aircraft Design, Systems and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2954.
Texte intégralARMENGAUD, F., R. DECHER, B. LAFOSSE et A. KOOPMAN. « One-dimensional modeling of hypersonic flight propulsion engines ». Dans Aircraft Design and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2026.
Texte intégralCASSIDY, P., et S. M. HALLEY. « Airframe/engine mechanical integration for hypersonic airbreathing aircraft ». Dans Aircraft Design and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3177.
Texte intégralCzysz, Paul. « For hypersonic design propulsion sharpens the focus ». Dans Aircraft Design, Systems, and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4012.
Texte intégralHARRIS, JR., ROY. « On the threshold - The outlook for supersonic and hypersonic aircraft ». Dans Aircraft Design and Operations Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2071.
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