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Статті в журналах з теми "Hypersonic aircraft design"
Alkaya, Can, Ashish Alex Sam, and Apostolos Pesyridis. "Conceptual Advanced Transport Aircraft Design Configuration for Sustained Hypersonic Flight." Aerospace 5, no. 3 (September 1, 2018): 91. http://dx.doi.org/10.3390/aerospace5030091.
Повний текст джерелаDai, Yalin, Yu Wang, Xiaoyu Xu, and Xiongqing Yu. "An Improved Method for Initial Sizing of Airbreathing Hypersonic Aircraft." Aerospace 10, no. 2 (February 18, 2023): 199. http://dx.doi.org/10.3390/aerospace10020199.
Повний текст джерелаKoptev, A. ""THEORETICAL ASPECTS OF STRENGTH AND THERMAL CONTROL OF HYPERSONIC AIRCRAFT"." National Association of Scientists 1, no. 66 (May 14, 2021): 54–60. http://dx.doi.org/10.31618/nas.2413-5291.2021.1.66.403.
Повний текст джерелаChen, Jie, Yan Lin, and Chang Peng Pan. "Hypersonic Aircraft Nonlinear Fault-Tolerant Controller Design." Applied Mechanics and Materials 494-495 (February 2014): 1056–59. http://dx.doi.org/10.4028/www.scientific.net/amm.494-495.1056.
Повний текст джерелаMorrell, Benjamin J., David J. Munk, Gareth A. Vio, and Dries Verstraete. "Development of a Hypersonic Aircraft Design Optimization Tool." Applied Mechanics and Materials 553 (May 2014): 847–52. http://dx.doi.org/10.4028/www.scientific.net/amm.553.847.
Повний текст джерелаWang, Zhiqiang, Anjing Zhang, Jia Pan, Weiguo Lu, and Yubiao Sun. "Fluid-Thermal Interaction Simulation of a Hypersonic Aircraft Optical Dome." Energies 15, no. 22 (November 17, 2022): 8619. http://dx.doi.org/10.3390/en15228619.
Повний текст джерелаYang, Jie, Song Ping Wu, and Wen Xin Hou. "A Method for Aerodynamic Characteristic Analysis of Hypersonic Aircraft Based on Response Surface Model." Applied Mechanics and Materials 477-478 (December 2013): 277–80. http://dx.doi.org/10.4028/www.scientific.net/amm.477-478.277.
Повний текст джерелаWang, Yuhui, Peng Shao, Qingxian Wu, and Mou Chen. "Reliability analysis for a hypersonic aircraft’s wing spar." Aircraft Engineering and Aerospace Technology 91, no. 4 (April 1, 2019): 549–57. http://dx.doi.org/10.1108/aeat-11-2017-0242.
Повний текст джерелаCastigliola, Luca, Flavia Causa, and Michele Grassi. "Navigation architecture for hypersonic aircraft." MATEC Web of Conferences 304 (2019): 04008. http://dx.doi.org/10.1051/matecconf/201930404008.
Повний текст джерелаJiao, Xin, and Ju Jiang. "Design of adaptive switching control for hypersonic aircraft." Advances in Mechanical Engineering 7, no. 10 (October 21, 2015): 168781401561046. http://dx.doi.org/10.1177/1687814015610465.
Повний текст джерелаДисертації з теми "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.
Повний текст джерелаFiorentini, Lisa. "Nonlinear Adaptive Controller Design For Air-breathing Hypersonic Vehicles." The Ohio State University, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=osu1274986563.
Повний текст джерелаDicara, 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.
Повний текст джерелаIncludes 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.
Повний текст джерелаSharifzadeh, 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.
Повний текст джерелаDoctorat 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.
Повний текст джерелаTancred, 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.
Повний текст джерелаКниги з теми "Hypersonic aircraft design"
Hani, Alkamhawi, and United States. National Aeronautics and Space Administration., eds. Hypersonic aircraft design. [Columbus, Ohio]: Ohio State University, 1990.
Знайти повний текст джерелаArdema, Mark D. Body weight of hypersonic aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Знайти повний текст джерелаA, Mackley Ernest, and Langley Research Center, eds. NASA's hypersonic research engine project: A review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаJ, Chattot J., Lawrence S. L, and United States. National Aeronautics and Space Administration., eds. 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Знайти повний текст джерелаGatlin, Gregory M. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. Hampton, Va: Langley Research Center, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Знайти повний текст джерелаAdvanced hypersonic aircraft design. [Columbus, Ohio]: Ohio State University, Aeronautical and Astronautical Engineering, 1992.
Знайти повний текст джерелаAeropropulsion '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.
Знайти повний текст джерелаЧастини книг з теми "Hypersonic aircraft design"
Merlen, A. "From the analytical theory to hypersonic aircraft design." In Asymptotic Modelling in Fluid Mechanics, 221–28. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/3-540-59414-0_69.
Повний текст джерелаYang, Zhiling, and Hongfei Sun. "Nonlinear Control Design of a Hypersonic Aircraft Using Sum-of-Squares Method." In 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.
Повний текст джерелаMartin, Katharina, Dennis Daub, Burkard Esser, Ali Gülhan, and Stefanie Reese. "Numerical Modelling of Fluid-Structure Interaction for Thermal Buckling in Hypersonic Flow." In 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.
Повний текст джерелаKossira, H., A. Bardenhagen, and W. Heinze. "An Integrated Computer-Program-System for the Preliminary Design of Advanced Hypersonic Aircraft (PrADO-Hy)." In Orbital Transport, 129–47. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-45720-3_9.
Повний текст джерелаGuo, Yixiang, Lifang Chen, and Yuhang Zhou. "A Review of the Development of Sealing Materials and Measurement and Control Simulation Technology for Typical Hypersonic Vehicle Positions." In Proceedings of the 2022 International Conference on Smart Manufacturing and Material Processing (SMMP2022). IOS Press, 2022. http://dx.doi.org/10.3233/atde220826.
Повний текст джерелаТези доповідей конференцій з теми "Hypersonic aircraft design"
JOHNSON, REUBEN. "Soviet applications for hypersonic vehicles." In Aircraft Design, Systems and Operations Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4507.
Повний текст джерелаCOONS, L. "Propulsion challenges for hypersonic flight." In Aircraft Systems, Design and Technology Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2620.
Повний текст джерелаTRIKHA, ARUN, and THOMAS CREIGHTON. "Crew escape system design for hypersonic vehicles." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2025.
Повний текст джерелаARDEMA, MARK, ERIC TERJESEN, and CATHY ROBERTS. "Body weight of advanced concept hypersonic aircraft." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3180.
Повний текст джерелаWARD, RICHARD, MARK LEAGUE, and EDDIE MOORE. "Assessment of a Soviet hypersonic transport." In Aircraft Design, Systems and Operations Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4506.
Повний текст джерелаCHAPUT, ARMAND. "Preliminary sizing methodology for hypersonic vehicles." In Aircraft Design, Systems and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2954.
Повний текст джерелаARMENGAUD, F., R. DECHER, B. LAFOSSE, and A. KOOPMAN. "One-dimensional modeling of hypersonic flight propulsion engines." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2026.
Повний текст джерелаCASSIDY, P., and S. M. HALLEY. "Airframe/engine mechanical integration for hypersonic airbreathing aircraft." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3177.
Повний текст джерелаCzysz, Paul. "For hypersonic design propulsion sharpens the focus." In Aircraft Design, Systems, and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4012.
Повний текст джерелаHARRIS, JR., ROY. "On the threshold - The outlook for supersonic and hypersonic aircraft." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2071.
Повний текст джерела