Academic literature on the topic 'Wing construction'

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Journal articles on the topic "Wing construction"

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Tarnowski, Andrzej. "Morphing wing with skin discontinuity – kinematic concept." Aircraft Engineering and Aerospace Technology 89, no. 4 (2017): 535–46. http://dx.doi.org/10.1108/aeat-11-2016-0208.

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Purpose This paper aims to describe the concept of morphing tailless aircraft with discontinuous skin and its preliminary kinematic solution. Project assumptions, next steps and expected results are briefly presented. Design/methodology/approach Multidisciplinary numerical optimization will be used to determine control allocation for wing segments rotation. Wing demonstrator will be fabricated and tested in wind tunnel. Results will be used in construction of flying model and design of its control system. Flight data of morphing demonstrator and reference aircraft will result in comparative an
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Richter, Charles, and Hod Lipson. "Untethered Hovering Flapping Flight of a 3D-Printed Mechanical Insect." Artificial Life 17, no. 2 (2011): 73–86. http://dx.doi.org/10.1162/artl_a_00020.

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This project focuses on developing a flapping-wing hovering insect using 3D-printed wings and mechanical parts. The use of 3D printing technology has greatly expanded the possibilities for wing design, allowing wing shapes to replicate those of real insects or virtually any other shape. It has also reduced the time of a wing design cycle to a matter of minutes. An ornithopter with a mass of 3.89 g has been constructed using the 3D printing technique and has demonstrated an 85-s passively stable untethered hovering flight. This flight exhibits the functional utility of printed materials for fla
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Irwin, A. J., and P. M. Render. "The influence of simulated missile warhead fragment damage on the aerodynamic characteristics of two-dimensional wings." Aeronautical Journal 117, no. 1194 (2013): 823–37. http://dx.doi.org/10.1017/s0001924000008472.

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AbstractThe paper describes a method of representing damage on a wing due to multiple warhead fragments, and investigates two of the key variables: fragment impact density and hole diameter. The aerodynamic effects of the damage were quantified by wind-tunnel tests on a two-dimensional wing at a Reynolds number of 5 × 105. The wing was of hollow construction with leading and trailing-edge spars. In all of the cases tested, simulated fragment damage resulted in significant lift losses, drag increases and pitching moment changes. Increasing fragment density or hole size resulted in greater effec
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Newman, D. J. S., and R. J. Wootton. "An Approach to the Mechanics of Pleating in Dragonfly Wings." Journal of Experimental Biology 125, no. 1 (1986): 361–72. http://dx.doi.org/10.1242/jeb.125.1.361.

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A structural engineering approach to the pleated wings of Odonata has been developed during a functional study of wing morphology in the group. The wing can be regarded as a folded plate structure within which each pleat-side acts as a deep plate-girder. Small cross-veins act as stiffeners within the girders, allowing the membrane to carry web shearing forces as pure tension, through a stressed-skin effect. Bending experiments confirm that the membrane significantly increases the rigidity of wing components. The properties of the membrane are unknown. It lacks birefringence, is very thin, and
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Breen, John E., Michael E. Kreger, Christopher D. White, and Gordon C. Clark. "Field evaluation and model test of a composite wing-girder bridge." Canadian Journal of Civil Engineering 14, no. 6 (1987): 753–62. http://dx.doi.org/10.1139/l87-113.

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This paper presents the key observations and conclusions from the evaluation of an innovative "loose-fit" composite, post-tensioned concrete wing-girder bridge proposed for an elevated interstate highway expansion in an urban environment. The evaluation program included both testing to destruction of a 1/2-scale model of a partial span as well as construction monitoring and field testing at service load levels of a full-scale prototype two-span bridge. Results of both construction measurements and loading tests were compared with analytical predictions. Laboratory tests showed the composite be
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YOSHIZU, Toshihiro. "DEVELOPMENT OF SCREW STEEL PIPE PILE WITH TOE WING HAVING AN INNER WING." AIJ Journal of Technology and Design 20, no. 45 (2014): 467–70. http://dx.doi.org/10.3130/aijt.20.467.

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Жданов, Дмитро, and Дмитро Зінченко. "Aerodynamic design of adaptive airplane wing of hybrid construction." MECHANICS OF GYROSCOPIC SYSTEMS, no. 29 (July 10, 2015): 84. http://dx.doi.org/10.20535/0203-377129201560714.

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WIELOCH, GRZEGORZ. "Low noise with wood milling "Airface" constructions." Annals of WULS, Forestry and Wood Technology 106 (January 15, 2019): 49–56. http://dx.doi.org/10.5604/01.3001.0013.7736.

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Low noise with wood milling"airface" constructions. The noise surrounds us everywhere, constituting a disruptive component of our lives. In the wood industry it is more than in other industries due to the specificity of wood processing carried out by high-speed tools. GUS data say that in 2012 as many as 53% of employees worked in noise. Hence the necessity of constant search for new methods of noise reduction. One of them is the use of a grooved surface patterned on the plumage of owls in the construction of milling heads. Their characteristic construction makes the flight of owls almost sile
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Arokiasami, Willson Amalraj, Prahlad Vadakkepat, and Abdullah Al Mamun. "Wingbeat Generation for a 15 DOF Flexible-Wing Aerial Vehicle Using Cosine Wave Functions." Unmanned Systems 05, no. 02 (2017): 115–27. http://dx.doi.org/10.1142/s230138501750008x.

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Birds and conventional airplanes control their flight in a different manner. Conventional airplanes maneuver themselves by means of moving surfaces, while birds can bend, twist and deform their wings and adapt to unforeseen conditions such as wind gusts. However, if planes can do exactly as the birds do they can gain agility, more lift, less drag while consuming less fuel. This work aims to address this issue. Therefore, approaches of wingbeat generation for a 15 DOF flexible-wing aerial vehicle are developed in this paper. A computationally cost-effective cosine wave function-based algorithm
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Horden, R. "The Wing Tower (Der "Wing Tower")." Stahlbau 69, no. 6 (2000): 466–68. http://dx.doi.org/10.1002/stab.200001490.

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Dissertations / Theses on the topic "Wing construction"

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Rahman, Selma, and Anujan Ranganathan. "Conceptual design and construction of a UAV wing structure." Thesis, KTH, Skolan för teknikvetenskap (SCI), 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-276681.

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This report presents the design of the wing structure for a UAV called Skywalker X8. A model of the UAV was given and analyzed to design a wing box structure that is twice the size of the current model, with "greener" technology and lightweight materials. The loads that act upon the UAV were simulated and thereafter analyzed with the help of the CFD program called Star CCM+. Modifications on the CAD model and the FEM simulations were performed in Siemens NX. Eight different combinations were tested from the following five materials: CFRP (carbon fiber reinforced polymer), LDPE (low density pol
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Skelton, Ian R. "Innovation in construction techniques for tall buildings." Thesis, Loughborough University, 2015. https://dspace.lboro.ac.uk/2134/19637.

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The skyline of many 'world cities' are defined and punctuated by tall buildings. The drivers for such dominant skylines range from land scarcity and social needs; high real estate values; commercial opportunity and corporate demand, through to metropolitan signposting. This fascination with tall buildings started with the patrician families who created the 11th Century skyline of San Gimignano by building seventy tower-houses (some up to 50m tall) as symbols of their wealth and power. This was most famously followed in the late 19th Century with the Manhattan skyline, then Dubai building the w
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Chabada, Martin. "Návrh křídla letounu UAV v kategorii do 600 kg." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-442849.

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The main aim of the this diploma thesis is the wing design of the UAV aircraft, including the appropriate material choice, calculation of the wing load and also strength analysis. Other goals include the design of the location and volume of fuel tanks, as well as the design of wingspan reduction after landing.
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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.

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The dissertation is focused on the large computational costs of integrated multidisciplinary design. Efficient techniques are developed to reduce the computational costs associated with integrated structural-aerodynamic design. First efficient methods for the calculations of the derivatives of the flexibility matrix and the aerodynamic influence coefficient matrix are developed. An adjoint method is used for the flexibility sensitivity, and a perturbation method is used for the aerodynamic sensitivity. Second a sequential optimization algorithm that employs approximate analysis methods is impl
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Strauch, Gregory J. "Integrated multi-disciplinary design of a sailplane wing." Thesis, Virginia Tech, 1985. http://hdl.handle.net/10919/45660.

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<p>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.</p> <p> Two design procedures are inve
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Polen, David M. "Integrated aerodynamic-structural design of a subsonic, forward- swept transport wing." Thesis, Virginia Tech, 1989. http://hdl.handle.net/10919/46059.

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<p>The 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.</p> <p>The pr
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Dewitz, Michael B. "The effect of a fillet on a wing/body junction flow." Thesis, Virginia Tech, 1988. http://hdl.handle.net/10919/43843.

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Brooks, W. G. "The design, construction and test of a postbuckled, carbon fibre reinforced plastic wing box." Thesis, Cranfield University, 1987. http://hdl.handle.net/1826/3292.

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A postbuckled, carbon fibre reinforced plastic (CFRP) wing box has been designed, manufactured and tested for an aerobatic light aircraft, the Cranfield Al. Methods of analysis have been evaluated including: i) Non-linear finite element analysis for the prediction o-f panel postbuckling. ii) A simpler technique based on an effective width method. This forms the core of a design program, 'oPTIMIST'. It predicts buckling loads, postbuckled reduced stiffness and overall column failure of co-cured hat stiffened panels. It then optimises the con-Figuration of a box beam for minimum weight. iii) The
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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.

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Past research at this university has proven the feasibility of the multi-disciplinary design of a complex system involving the complete interaction of aerodynamics and structural mechanics. Critical to this design process, is the ability to accurately and efficiently calculate the sensitivities of the involved quantities (such as drag and dynamic pressure) with respect to the design variables. These calculations had been addressed in past research, but it was felt that insufficient accuracy had been obtained. The focus of this research was to improve the accuracy of these sensitivity calculati
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Rohl, Peter Jurgen. "A multilevel decomposition procedure for the preliminary wing design of a high-speed civil transport aircraft." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/11827.

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Books on the topic "Wing construction"

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Selberg, Bruce P. Aerodynamic-structural study of canard wing, dual wing and conventional wing systems for general aviation applications. NASA Langley Research Center, 1985.

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Fighter wing: A guided tour of an Airforce Combat wing. Berkley Books, 1995.

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Wood, Richard M. The natural flow wing-design concept. Langley Research Center, 1992.

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Clancy, Tom. Fighter wing: A guided tour of an Air Force combat wing. Berkley Books, 1995.

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Clancy, Tom. Fighter wing: A guided tour of an Air Force combat wing. Berkley Books, 2004.

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Fighter wing: A guided tour of an Air Force combat wing. HarperCollins, 1995.

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Valasek, John. Morphing aerospace vehicles and structures. John Wiley & Sons, 2012.

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American Institute of Aeronautics and Astronautics, ed. Morphing aerospace vehicles and structures. John Wiley & Sons, 2012.

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Wrong and dangerous: Ten right-wing myths about the constitution. Rowman & Littlefield, 2012.

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Merlin, Peter W. A New twist in flight research: The F-18 active aeroelastic wing project. National Aeronautics and Space Administration, Aeronautics Research Mission Directorate, 2013.

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Book chapters on the topic "Wing construction"

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Moss, David. "The Construction of Judicial Accounts." In The Politics of Left-Wing Violence in Italy, 1969–85. Palgrave Macmillan UK, 1989. http://dx.doi.org/10.1007/978-1-349-20249-2_5.

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Brooks, W. G. "The Construction of a Postbuckled Carbon Fibre Wing Box." In Composite Structures 4. Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3455-9_13.

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Siim, Birte, and Susi Meret. "Right-wing Populism in Denmark: People, Nation and Welfare in the Construction of the ‘Other’." In The Rise of the Far Right in Europe. Palgrave Macmillan UK, 2016. http://dx.doi.org/10.1057/978-1-137-55679-0_5.

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Berend, Ivan T. "Is the European Union a neoliberal construction that deserves to be destroyed? A debate with left-wing attacks." In Against European Integration. Routledge, 2019. http://dx.doi.org/10.4324/9780429200458-10.

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Gill, Clare. "Reading the ‘Religion of Socialism’: Olive Schreiner, the Labour Church and the Construction of Left-wing Reading Communities in the 1890s." In The History of Reading, Volume 2. Palgrave Macmillan UK, 2011. http://dx.doi.org/10.1057/9780230316799_4.

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Qu, Yingying, and Sai On Cheung. "Logrolling “Win–Win” Settlement in Construction Dispute Mediation." In Construction Dispute Research. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-04429-3_20.

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Hau, Erich, Jens Langenbrinck, and Wolfgang Palz. "The WEGA Wind Turbines — Design and Construction." In WEGA Large Wind Turbines. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52129-4_3.

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Bahadori, Mehdi N., Alireza Dehghani-sanij, and Ali Sayigh. "Designing, Constructing, and Testing Conventional Baudgeers and New Designs." In Wind Towers. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-05876-4_7.

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Wisser, A., and W. Nachtigall. "Biomechanical Aspects of the Wing Joints in Flies, Especially in Calliphora erythrocephala." In Constructional Morphology and Evolution. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76156-0_14.

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Borri, Claudio, Paolo Biagini, and Enzo Marino. "Large wind turbines in earthquake areas: structural analyses, design/construction & in-situ testing." In Environmental Wind Engineering and Design of Wind Energy Structures. Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0953-3_7.

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Conference papers on the topic "Wing construction"

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Thompson, Daniel, Joshuo Feys, Michael Filewich, Sharif Abdel-Magid, Dennis Dalli, and Fumitaka Goto. "The Design and Construction of a Blended Wing Body UAV." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-841.

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Manzo, Justin E., Emily A. Leylek, and Ephrahim Garcia. "Drawing Insight From Nature: A Bat Wing for Morphing Aircraft." In ASME 2008 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2008. http://dx.doi.org/10.1115/smasis2008-613.

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Being the only flying mammal, bats have evolved unique flight devices affording them high maneuverability and efficiency despite their low flight speeds. By selecting bats of three different ecological niches — a highly efficient fishing bat, a nimble insectivorous forager, and a large soaring bat of the ‘flying fox’ family — passive wing shapes can be demonstrated as capable of attaining very different aerodynamic performance characteristics. The aerodynamics of man-made equivalents to these wing shapes, using thin airfoils rather than skeleton and membrane construction, are studied both comp
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Onishi, Ryoichi, Toshiya Kimura, Zhihong Guo, and Toshiyuki Iwamiya. "Computational aero-structural dynamics for wing with skin-spar-rib construction." In 18th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4225.

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Andaste, Yosua Sepri, Muhammad Aldo Aditiya Nugroho, R. S. Brian Benyamin, Bambang Riyanto Trilaksono, and Agoes Moelyadi. "Design and construction of flapping wing micro aerial vehicle robot platform." In 2017 7th IEEE International Conference on System Engineering and Technology (ICSET). IEEE, 2017. http://dx.doi.org/10.1109/icsengt.2017.8123444.

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Olejnik, A., L. Kiszkowiak, M. Jędrak, J. Milczarczyk, and A. Dziubiński. "Crash Analysis of Wing of Large Airplane with a Tree." In 17th Biennial International Conference on Engineering, Science, Construction, and Operations in Challenging Environments. American Society of Civil Engineers, 2021. http://dx.doi.org/10.1061/9780784483381.014.

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Aguillon Balderas, Nestor Abraham, Gerardo Emanuel Cardona Sanchez, Jessica Jazmin Maldonado Ramos, Carlos Antonio Tovar Garcia, and Alejandro J. Malo Tamayo. "Construction and instrumentation of a fixed wing aircraft guillow's aeronca champion 85." In 2015 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS). IEEE, 2015. http://dx.doi.org/10.1109/red-uas.2015.7441031.

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Ding, Menglong, and Wieslaw Binienda. "Numerical Study of a Transport Aircraft Wing Impact with a Birch Tree." In 17th Biennial International Conference on Engineering, Science, Construction, and Operations in Challenging Environments. American Society of Civil Engineers, 2021. http://dx.doi.org/10.1061/9780784483381.007.

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Henry, Jonathon, David Schwartz, Michael Soukup, and Aaron Altman. "Design, Construction, and Testing of a Folding-Wing, Tube-Launched Micro Air Vehicle." In 43rd AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-1451.

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Salistean, Adrian, Carmen Mihai, Doina Toma, and Sabina Olaru. "Theoretical and practical aspects of the design phase for a single skin textile wing." In The 8th International Conference on Advanced Materials and Systems. INCDTP - Leather and Footwear Research Institute (ICPI), Bucharest, Romania, 2020. http://dx.doi.org/10.24264/icams-2020.iii.16.

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This paper depicts the early phase in the research development for an integrated support system tailored for emergency response actions and remote sensing. The support system is envisioned as an integrated Unmanned Aerial System (UAS) system that consists of one or more ultralight multifunctional aerial units with a configuration that can be adapted to the nature of the intervention: monitoring, mapping, observation and logistics etc. These aerial units comprise of para-motor type UAVs that use textile paraglider wings of a special design. The paper summarizes the basic materials used in the c
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Abeysinghe, Asith, Shameera Abeysiriwardena, Roshan Nanayakkarawasam, Walallawita Wimalsiri, Thilina Dulantha Lalitharatne, and Salinda Tennakoon. "Development of a numerically controlled hot wire foam cutting machine for wing mould construction." In 2016 Moratuwa Engineering Research Conference (MERCon). IEEE, 2016. http://dx.doi.org/10.1109/mercon.2016.7480116.

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Reports on the topic "Wing construction"

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URS CORP OAKLAND CA. Environmental Assessment of Short-Term Construction Projects at the 150th Fighter Wing, New Mexico Air National Guard, Kirtland Air Force Base, New Mexico. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada639962.

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Worachek, Alden, and Forest Button. Bethel Wind Energy Construction Project. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1607624.

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Worachek, Alden, and Forest Button. Pitka's Point/St. Mary's Wind Energy Construction Project. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1607457.

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McMillan, Andy. Cherokee Wind Energy Development - Feasibility and Pre-Construction Studies. Office of Scientific and Technical Information (OSTI), 2017. http://dx.doi.org/10.2172/1395350.

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Connolly, Michael. Pre-construction Activities for Phase 1 of Shu'luuk Wind Project. Office of Scientific and Technical Information (OSTI), 2015. http://dx.doi.org/10.2172/1208019.

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DeRenzis, A., and V. Kochkin. High-R Walls for New Construction Structural Performance. Wind Pressure Testing. Office of Scientific and Technical Information (OSTI), 2013. http://dx.doi.org/10.2172/1219901.

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DeRenzis, A., and V. Kochkin. High-R Walls for New Construction Structural Performance: Wind Pressure Testing. Office of Scientific and Technical Information (OSTI), 2013. http://dx.doi.org/10.2172/1067930.

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Matlack, Raymond S. Wind Energy and Wildlife Pre- and Post-Construction Project at Pantex Plant. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1416956.

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Ligotke, M. W., G. W. Dennis, and L. L. Bushaw. Wind tunnel tests of biodegradable fugitive dust suppressants being considered to reduce soil erosion by wind at radioactive waste construction sites. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10190697.

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Dagher, Habib, Anthony Viselli, Andrew Goupee, Richard Kimball, and Christopher Allen. The VolturnUS 1:8 Floating Wind Turbine: Design, Construction, Deployment, Testing, Retrieval, and Inspection of the First Grid-Connected Offshore Wind Turbine in US. Office of Scientific and Technical Information (OSTI), 2017. http://dx.doi.org/10.2172/1375022.

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