Literatura académica sobre el tema "Integrated Wing Design"
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Artículos de revistas sobre el tema "Integrated Wing Design"
Rais-Rohani, M., R. T. Haftka, B. Grossman y E. R. Unger. "Integrated aerodynamic-structural-control wing design". Computing Systems in Engineering 3, n.º 6 (diciembre de 1992): 639–50. http://dx.doi.org/10.1016/0956-0521(92)90015-b.
Texto completoOleinikov, Alexander Ivanovich. "Integrated Design of Wing Panel Manufacture Processes". Key Engineering Materials 554-557 (junio de 2013): 2175–86. http://dx.doi.org/10.4028/www.scientific.net/kem.554-557.2175.
Texto completoGrossman, B., Z. Gurdal, G. J. Strauch, W. M. Eppard y R. T. Haftka. "Integrated aerodynamic/structural design of a sailplane wing". Journal of Aircraft 25, n.º 9 (septiembre de 1988): 855–60. http://dx.doi.org/10.2514/3.45670.
Texto completoGrossman, B., R. T. Haftka, P. J. Kao, D. M. Polen, M. Rais-Rohani y J. Sobieszczanski-Sobieski. "Integrated aerodynamic-structural design of a transport wing". Journal of Aircraft 27, n.º 12 (diciembre de 1990): 1050–56. http://dx.doi.org/10.2514/3.45980.
Texto completoSALISTEAN, ADRIAN, DOINA TOMA, IONELA BADEA y MIHAELA JOMIR. "Design of a small-scale UAV textile wing fluid-structure numerical modelling". Industria Textila 72, n.º 04 (1 de septiembre de 2021): 449–53. http://dx.doi.org/10.35530/it.072.04.1844.
Texto completoPatil, Ankur S. y Emily J. Arnold. "Sensor-Driven Preliminary Wing Ground Plane Sizing Approach and Applications". International Journal of Aerospace Engineering 2018 (2 de julio de 2018): 1–15. http://dx.doi.org/10.1155/2018/6378635.
Texto completoMaute, K. y G. W. Reich. "Integrated Multidisciplinary Topology Optimization Approach to Adaptive Wing Design". Journal of Aircraft 43, n.º 1 (enero de 2006): 253–63. http://dx.doi.org/10.2514/1.12802.
Texto completoBotez, R. M., M. J. Tchatchueng Kammegne y L. T. Grigorie. "Design, numerical simulation and experimental testing of a controlled electrical actuation system in a real aircraft morphing wing model". Aeronautical Journal 119, n.º 1219 (septiembre de 2015): 1047–72. http://dx.doi.org/10.1017/s0001924000011131.
Texto completoZhang, Gong Ping, Zhi Zhong Liao, Chao Yang Duan y Peng Ju Wang. "Optimal Design of Configuration Change Program for Tactical Missile with Morphing Wings". Applied Mechanics and Materials 101-102 (septiembre de 2011): 410–13. http://dx.doi.org/10.4028/www.scientific.net/amm.101-102.410.
Texto completode Mattos, Bento Silva, Paulo Jiniche Komatsu y Jesuíno Takachi Tomita. "Optimal wingtip device design for transport airplane". Aircraft Engineering and Aerospace Technology 90, n.º 5 (2 de julio de 2018): 743–63. http://dx.doi.org/10.1108/aeat-07-2015-0183.
Texto completoTesis sobre el tema "Integrated Wing Design"
Unger, Eric Robert. "Integrated aerodynamic-structural wing design optimization". Diss., This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09042008-063104/.
Texto completoStrauch, Gregory J. "Integrated multi-disciplinary design of a sailplane wing". Thesis, Virginia Tech, 1985. http://hdl.handle.net/10919/45660.
Texto completoThe objective of this research is to investigate the techniques and payoffs of integrated aircraft design. Lifting line theory and beam theory are used for the analysis of the aerodynamics and the structures of a composite sailplane wing. The wing is described by 33 - 34 design variables which involve the planform geometry, the twist distribution, and thicknesses of the spar caps, spar webs, and the skin at various stations along the wing. The wing design must satisfy 30 â 31 aeroelastic, structural, aerodynamic, and performance constraints.
Two design procedures are investigated. The first, referred to as the iterative, sequential procedure, involves optimizing the aerodynamic design for maximum average cross-country speed at E1 constant structural weight, and then optimizing the the structural design of the resulting wing geometry for minimum weight. This value is then used in another aerodynamic optimization, and the process continues iteratively until the weight converges. The other procedure, the integrated one, simultaneously optimizes the aerodynamic and the structural design variables for either maximum average cross-country speed or minimum weight.
The integrated procedure was able to improve the value of the objective function obtained by the iterative procedure in all cases. This shows The objective of this research is to investigate the techniques and payoffs of integrated aircraft design. Lifting line theory and beam theory are used for the analysis of the aerodynamics and the structures of a composite sailplane wing. The wing is described by 33 - 34 design variables which involve the planform geometry, the twist distribution, and thicknesses of the spar caps, spar webs, and the skin at various stations along the wing. The wing design must satisfy 30 â 31 aeroelastic, structural, aerodynamic, and performance constraints. Two design procedures are investigated. The first, referred to as the iterative, sequential procedure, involves optimizing the aerodynamic design for maximum average cross-country speed at E1 constant structural weight, and then optimizing the the structural design of the resulting wing geometry for minimum weight. This value is then used in another aerodynamic optimization, and the process continues iteratively until the weight converges. The other procedure, the integrated one, simultaneously optimizes the aerodynamic and the structural design variables for either maximum average cross-country speed or minimum weight.
The integrated procedure was able to improve the value of the objective function obtained by the iterative procedure in all cases. This shows that definite benefits can be gained from taking advantage of aerodynamic/structural interactions during the design process.
Master of Science
Kao, Pi-Jen. "Efficient methods for integrated structural-aerodynamic wing optimum design". Diss., Virginia Polytechnic Institute and State University, 1989. http://hdl.handle.net/10919/54211.
Texto completoPh. D.
MAININI, LAURA. "Multidisciplinary and multi-fidelity optimization environment for wing integrated design". Doctoral thesis, Politecnico di Torino, 2012. http://hdl.handle.net/11583/2500000.
Texto completoPolen, David M. "Integrated aerodynamic-structural design of a subsonic, forward- swept transport wing". Thesis, Virginia Tech, 1989. http://hdl.handle.net/10919/46059.
Texto completoThe introduction of composite materials and the ability to tailor these materials to improve aerodynamic and structural performance is having a distinct effect upon aircraft design. In order to optimize the efficiency of the design procedure, a design process which is more integrated than the traditional approach is required. Currently the utilization of such design procedures produces enormous computational costs. An ongoing effort to reduce these costs is the development of efficient methods for cross-disciplinary sensitivities and approximate optimization techniques.
The present research concentrates on investigating the integrated design optimization of a subsonic, forward-swept transport wing. A modular sensitivity approach for calculating the cross-sensitivity derivatives is employed. These derivatives are then used to guide the optimization process. The optimization process employed is an approximate technique due to the complexity of the analysis procedures. These optimization results are presented and the impact of the modular technique is discussed.
Master of Science
Unger, Eric Robert. "Computational aspects of the integrated multi-disciplinary design of a transport wing". Thesis, Virginia Tech, 1990. http://hdl.handle.net/10919/42125.
Texto completoMaster of Science
Bortolotti, Pietro [Verfasser]. "Integrated Design of Wind Turbines / Pietro Bortolotti". München : Verlag Dr. Hut, 2018. http://d-nb.info/1166482456/34.
Texto completoZhang, Hui. "Wind turbine adaptive blade integrated design and analysis". Thesis, Northumbria University, 2013. http://nrl.northumbria.ac.uk/21439/.
Texto completoRogers, Mary C. M. "Control aspects of integrated design of wind turbines : a foundation". Thesis, University of Strathclyde, 1998. http://oleg.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=21367.
Texto completoPerez, Damas Carlos Emilio. "Design of an airborne wind energy (AWE) research platform". Thesis, Massachusetts Institute of Technology, 2018. http://hdl.handle.net/1721.1/118530.
Texto completoThesis: S.M., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2018.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 121-126).
Airborne wind energy (AWE) technologies have the potential to become a dominant source of clean electricity generation and help humanity reach many of the key sustainable development goals (SDGs) established by the United Nations as part of the 2030 Agenda for Sustainable Development. AWE systems eliminate the need for a tower, large blades and substantial foundations used in modern wind turbines and replace it with a wing (i.e. kite or glider aircraft) tethered to the ground. This technology can reach higher-altitude winds which is an untapped source of clean and highly abundant energy with the potential to power civilization 100 times over. As part of this work, an AWE research platform has been designed and developed based on a concept that emphasizes low-complexity, safety and low-cost. This research platform can be used to evaluate different sensor frameworks, airfoil/tether designs, control systems and optimal operational strategies for AWE systems operating under lift mode. A first-order techno-economic analysis was also performed to assess the cost and technical feasibility of developing a small-scale AWE system for distributed generation applications. In addition to estimating the approximate cost of the system, the analysis also determines the potential power generated by a specific AWE system design operating at a maximum elevation of 152 meters, to comply with existing regulation. The results of the techno-economic analysis suggest that small-scale AWE systems have the potential to produce electricity at a much lower cost than small-wind turbines of the same rated capacity.
by Carlos Emilio Perez Damas.
S.M. in Engineering and Management
S.M.
Libros sobre el tema "Integrated Wing Design"
United States. National Aeronautics and Space Administration., ed. Integrated design and manufacturing for the high speed civil transport: Preliminary design methodology and optimization for an HSCT Nacelle/Wing configuration : final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Buscar texto completoBartoli, Gianni, Francesco Ricciardelli, Anna Saetta y Vincenzo Sepe, eds. Performance of Wind Exposed Structures. Florence: Firenze University Press, 2006. http://dx.doi.org/10.36253/978-88-6453-156-4.
Texto completoCenter, Langley Research, ed. Design of the wind tunnel model communication controller board. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoGevorkian, Peter. Alternative energy systems in building design. New York: McGraw-Hill, 2010.
Buscar texto completoAlternative energy systems in building design. New York: McGraw-Hill, 2010.
Buscar texto completoGevorkian, Peter. Sustainable Energy Systems in Architectural Design. New York: McGraw-Hill, 2006.
Buscar texto completoSustainable energy systems in architectural design: A blueprint for green building. New York: McGraw-Hill, 2006.
Buscar texto completoYuan, Chao. Urban Wind Environment: Integrated Climate-Sensitive Planning and Design. Springer, 2018.
Buscar texto completoYuan, Chao. Urban Wind Environment: Integrated Climate Sensitive Planning and Design. Springer Singapore Pte. Limited, 2018.
Buscar texto completoDoquang, Mailan S. The Lithic Garden. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780190631796.001.0001.
Texto completoCapítulos de libros sobre el tema "Integrated Wing Design"
Lukens, Jennifer M., Gregory W. Reich y Brian Sanders. "Wing Mechanization Design and Wind Tunnel Testing for a Perching Micro Air Vehicle". En Emboding Intelligence in Structures and Integrated Systems, 589–94. Stafa: Trans Tech Publications Ltd., 2008. http://dx.doi.org/10.4028/3-908158-13-3.589.
Texto completoWunderlich, Tobias y Lars Reimer. "Integrated Process Chain for Aerostructural Wing Optimization and Application to an NLF Forward Swept Composite Wing". En Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 3–33. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-72020-3_1.
Texto completoDenieul, Yann, Joël Bordeneuve, Daniel Alazard, Clément Toussaint y Gilles Taquin. "Integrated Design and Control of a Flying Wing Using Nonsmooth Optimization Techniques". En Advances in Aerospace Guidance, Navigation and Control, 475–89. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_27.
Texto completoSoukal, Ivan y Aneta Bartuskova. "WINE: Web Integrated Navigation Extension; Conceptual Design, Model and Interface". En Computational Collective Intelligence, 462–72. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-67074-4_45.
Texto completoHarbola, Shubhi, Martin Storz y Volker Coors. "Augmented Reality for Windy Cities: 3D Visualization of Future Wind Nature Analysis in City Planning". En iCity. Transformative Research for the Livable, Intelligent, and Sustainable City, 241–50. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-92096-8_15.
Texto completoUzunoglu, E. y C. Guedes Soares. "An integrated design approach for a self-float capable tension leg platform for wind energy". En Developments in Maritime Technology and Engineering, 673–81. London: CRC Press, 2021. http://dx.doi.org/10.1201/9781003216599-71.
Texto completoKoitz, Roxane, Johannes Lüftenegger y Franz Wotawa. "Model-Based Diagnosis in Practice: Interaction Design of an Integrated Diagnosis Application for Industrial Wind Turbines". En Advances in Artificial Intelligence: From Theory to Practice, 440–45. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-60042-0_48.
Texto completoZillner, Sonja. "Business Models and Ecosystem for Big Data". En The Elements of Big Data Value, 269–88. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-68176-0_11.
Texto completoBeghdadi, M., K. Kouzi y A. Ameur. "New Design of an Optimized Synergetic Control by Hybrid BFO-PSO for PMSG Integrated in Wind Energy Conversion System Using Variable Step HCS Fuzzy MPPT". En Lecture Notes in Networks and Systems, 30–40. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-37207-1_4.
Texto completoYawson, David O., Michael O. Adu, Paul A. Asare y Frederick A. Armah. "Multifunctional Landscape Transformation of Urban Idle Spaces for Climate Resilience in Sub-Saharan Africa". En African Handbook of Climate Change Adaptation, 1–27. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-42091-8_214-1.
Texto completoActas de conferencias sobre el tema "Integrated Wing Design"
RAIS-ROHANI, M., R. HAFTKA, B. GROSSMAN y E. UNGER. "Integrated aerodynamic-structural-control wing design". En 4th Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-4694.
Texto completoShi, Guoqin, Guillaume Renaud, Fengxian Zhang, Suzhen Chen y XinFeng Yang. "Integrated Wing Design with Three Disciplines". En 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-5405.
Texto completoGROSSMAN, B., R. HAFTKA, P. J. KAO, D. POLEN, M. RAIS-ROHANI y J. SOBIESZCZANSKI-SOBIESKI. "Integrated aerodynamic-structural design of a transport wing". En Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2129.
Texto completoHenderson, Joseph, Terrence Weisshaar y Brian Sanders. "Integrated wing design with adaptive control surfaces". En 19th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-1428.
Texto completoGROSSMAN, B., Z. GURDAL y R. HAFTKA. "Integrated aerodynamic/structural design of a sailplane wing". En Aircraft Systems, Design and Technology Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2623.
Texto completoMiyakawa, Junichi, Takeshi Ohnuki y Nobuhiko Kamiya. "Aero-Structural Integrated Design of Forward Swept Wing". En International Pacific Air & Space Technolgy Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1991. http://dx.doi.org/10.4271/912021.
Texto completoMainini, Laura, Massimiliano Mattone, Marco Di Sciuva y Paolo Maggiore. "Multidisciplinary Integrated design Environment for Aircraft Wing Sizing". En 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-9190.
Texto completoBorer, Nicholas K. y Mark D. Moore. "Integrated Propeller-Wing Design Exploration for Distributed Propulsion Concepts". En 53rd AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1672.
Texto completoHolness, Alex, Ella Steins, Hugh Bruck, Martin Peckerar y S. K. Gupta. "Performance Characterization of Multifunctional Wings With Integrated Flexible Batteries for Flapping Wing Unmanned Air Vehicles". En ASME 2016 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/detc2016-60379.
Texto completoCole, Julia A., Travis D. Krebs, Devin F. Barcelos, Alton Yeung y Goetz Bramesfeld. "On the Integrated Aerodynamic Design of a Propeller-Wing System". En AIAA Scitech 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2300.
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