Academic literature on the topic 'Commercial Aircraft Design And Construction'

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Journal articles on the topic "Commercial Aircraft Design And Construction"

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Li, Da Chuan, Nong Cheng, Peng Cheng, and Jing Yan Song. "Design and Development of an Integrated Flight Planning and Rehearsal System Based on GIS and Navigation Database." Applied Mechanics and Materials 232 (November 2012): 169–77. http://dx.doi.org/10.4028/www.scientific.net/amm.232.169.

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In modern civil aviation operations, the effective performance of pre-flight flight planning is the key of a safe flight, and the changing air traffic environment often requires modifying the pre-determined flight plan or even en route re-planning. This paper proposes an integrated system framework for the construction, re-planning, rehearsal and evaluation of computerized flight plans (CFP): the flight plan management and rehearsal system (FMRS). It provides interactive, graphic user interface - based ways of constructing flight routes using the navigation database and geographic information
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Ghiţescu, Ion-Marius, Maria Luminita Scutaru, Marilena Ghiţescu, Paul Nicolae Borza, and Marin Marin. "New Command Mechanism of Flaps and Wings of a Light Sport Aircraft." Symmetry 13, no. 2 (2021): 221. http://dx.doi.org/10.3390/sym13020221.

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Commercial aircraft have well-designed and optimized systems, the result of a huge experience in the field, due to the large fleet of aircraft in operation. For light, utility, or sports aircraft, with a multitude of shapes, tasks, and construction types, there are different solutions that seek to best meet the requirements of the designed aircraft. In this sense, for a sport plane, an increased maneuverability is desired, and the system that controls flaps and wing must be properly designed. A new flap mechanism command solution is proposed and justified in the paper, for use in sports and re
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Chenxi, L. I., H. U. Ying, and H. E. Liyan. "Exploration and optimization on the usage of micro-perforated panels as trim panels in commercial aircrafts." Noise Control Engineering Journal 68, no. 1 (2020): 87–100. http://dx.doi.org/10.3397/1/37687.

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Micro-perforated panels (MPPs), as an alternative to porous materials for sound absorption, have been commonly used in electronic industries and aircraft engines but are barely used in aircraft cabins. The effect of MPPs on the sound insulation and absorption properties of aircraft cabin panels has been investigated in this article. Theoretical modeling has been conducted on an aircraft cabin panel structure with a trim panel replaced by an MPP trim panel, using the transfer matrix method and the classic MPP theory. It is indicated by the theoretical results that, although the sound transmissi
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White, Greg. "Comparing the Cost of Rigid and Flexible Aircraft Pavements Using a Parametric Whole of Life Cost Analysis." Infrastructures 6, no. 8 (2021): 117. http://dx.doi.org/10.3390/infrastructures6080117.

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The construction and maintenance costs, as well as the residual value, were calculated for structurally equivalent rigid and flexible airfield pavements, for a range of typical commercial aircraft, as well as a range for typical subgrade conditions. Whole of life cost analysis was performed for a range of analysis periods, from 40 years to 100 years. For the standard 40-year analysis period and a residual value based on rigid pavement reconstruction, the rigid pavements had a 40% to 105% higher whole of life cost than equivalent flexible pavements, although this comparison is limited to the pa
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Samir, Peter, and George Morcous. "Precast Prestressed Concrete Truss-Girder for Roof Applications." Journal of Structures 2014 (December 14, 2014): 1–13. http://dx.doi.org/10.1155/2014/524156.

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Steel trusses are the most popular system for supporting long-span roofs in commercial buildings, such as warehouses and aircraft hangars. There are several advantages of steel trusses, such as lightweight, ease of handling and erection, and geometric flexibility. However, they have some drawbacks, such as high material and maintenance cost, and low fire resistance. In this paper, a precast concrete truss is proposed as an alternative to steel trusses for spans up to 48 m (160 ft) without intermediate supports. The proposed design is easy to produce and has lower construction and maintenance c
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Fuad, O. "SPACE TOURISM: PRE-FLIGHT PREPARATION AS OBJECT DESIGNING." Technical Aesthetics and Design Research 2, no. 4 (2021): 42–55. http://dx.doi.org/10.34031/2687-0878-2020-2-4-42-53.

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Today the space industry has a powerful technical, theoretical and practical base. However, until nowadays, sending a man into space has only a professional focus (except in some cases). A significant number of people who want to make a space flight is confirmed by statistical studies. The travel business is just starting to offer this service. The main directions of commercial development of the industry are the followings: the creation of infrastructure facilities, specialized aircraft, the development of a training system for "space" tourists, the creation of an appropriate subject-spatial
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Ang, Linus, Yong Koh, and Heow Lee. "Plate-Type Acoustic Metamaterials: Experimental Evaluation of a Modular Large-Scale Design for Low-Frequency Noise Control." Acoustics 1, no. 2 (2019): 354–68. http://dx.doi.org/10.3390/acoustics1020019.

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For industrial applications, the scalability of a finalised design is an important factor to consider. The scaling process of typical membrane-type acoustic metamaterials may pose manufacturing challenges such as stress uniformity of the membrane and spatial consistency of the platelet. These challenges could be addressed by plate-type acoustic metamaterials with an internal tonraum resonator. By adopting the concept of modularity in a large-scale design (or meta-panel), the acoustical performance of different specimen configurations could be scaled and modularly combined. This study justifies
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Beneke, Jeremy, Byron Jones, and Mohammad Hosni. "Fine particle dispersion in a commercial aircraft cabin." HVAC&R Research 17, no. 1 (2011): 107–17. http://dx.doi.org/10.1080/10789669.2011.543255.

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Lee, D. I., and W. Jin. "Prediction of Commercial Aircraft Price Using the COC & Aircraft Design Factors." Procedia Engineering 67 (2013): 70–77. http://dx.doi.org/10.1016/j.proeng.2013.12.006.

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Braune, Rolf J., and R. Curtis Graeber. "Human-Centered Designs in Commercial Transport Aircraft." Proceedings of the Human Factors Society Annual Meeting 36, no. 15 (1992): 1118–22. http://dx.doi.org/10.1518/107118192786749702.

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Based on airline pilot surveys, industry committees and workshops, conducted on advanced technology “glass cockpit” airplanes, concerns have been raised about the application and long-term effects of automation technologies. It has been pointed out that purely technology-driven designs had resulted in unintended and unforeseen negative consequences. In order to counter this trend it has been proposed to shift the focus from technology-centered designs to what has become known as human-centered design. There are three primary objectives within a human-centered design philosophy: (1) the design
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Dissertations / Theses on the topic "Commercial Aircraft Design And Construction"

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Markish, Jacob 1978. "Valuation techniques for commercial aircraft program design." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/16871.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.<br>Includes bibliographical references (p. 147-149).<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>This research considers the commercial aircraft design process from the perspective of program value. Whereas traditionally, the conceptual design of aircraft has often focused on minimum weight, or sometimes minimum cost, this approach demonstrates the feasibility and usefulness of design base
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Peoples, Ryan E. "Value-based multidisciplinary optimization for commercial aircraft program design." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/32117.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>Includes bibliographical references (p. 115-118).<br>Traditional commercial aircraft design attempts to achieve improved performance and reduced operating costs by minimizing maximum takeoff weight, but this approach (does not guarantee the financial viability of the program to the manufacturer. Improved design practices would take into account n
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Gómez, González Victor, and Collado Emilio José Izquierdo. "The Cormoran project: a new concept in commercial aircraft design." Thesis, KTH, Aerodynamik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-121357.

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This paper presents a new revolutionary design in commercial aircraft: the conven-tional vertical and horizontal tails are not present as generally known, and their contri-bution to the manoeuvering of the aircraft, namely the presence of the rudder and theelevators, is achieved by locating them at the wingtips and in the canard, respectively.Substituting the horizontal tail with the canard, the possibility of dividing the fuel be-tween the wing (where it is located conventionally) and the canard allows the pilot tochange the center of gravity during the ight with more freedom, while the eect
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Vera, Anders Hanyo. "User Preferred Trajectories in Commercial Aircraft Operation: Design and Implementation." Licentiate thesis, KTH, Aeronautical and Vehicle Engineering, 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4454.

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<p>This report describes how an aircraft creates and flies its User Preferred Trajectory from take-off to landing, based on the objectives and constraints the aircraft is subjected to from a technological and operational viewpoint.</p><p>A basic description of commercial aircraft operation is given, with an emphasis on identifying the different stakeholders (Air Navigation Service Providers, Airline Operation Center, Pilot/Aircraft, Airport and Civil Aviation Authority). A general description of Instrument Flight Rules operations is also given, together with an explanation of the capabilities
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Vera, Anders Hayo. "User preferred trajectories in commercial aircraft operation : design and implementation /." Stockholm : Institutionen för farkost och flyg, Kungliga Tekniska högskolan, 2007. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4454.

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Vora, Jay Abhilash. "Blended Wing Design Considerations for A Next Generation Commercial Aircraft." Wright State University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1557920109832295.

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Rowles, Craig M. 1962. "System integration analysis of a large commercial aircraft engine." Thesis, Massachusetts Institute of Technology, 1999. http://hdl.handle.net/1721.1/9753.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, 1999.<br>10912289<br>Includes bibliographical references (p. 93-94).<br>In this thesis we develop and demonstrate a method, called a System Integration Analysis, to produce a comprehensive understanding of the activities Integrated Product Teams (IPTs) perform in designing and developing a large complex product or system. The methodology is applied to an existing product or system whose physical architecture can be partitioned into comparable sections, or chunks, as the IPTs who design and develop it. I
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Jones, Natasha Ruth. "Designing shock control bumps for transonic commercial aircraft." Thesis, University of Cambridge, 2017. https://www.repository.cam.ac.uk/handle/1810/275993.

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Shock control bumps (SCBs) are considered promising flow control devices for transonic commercial aircraft. By generating a λ-shock structure, 2D SCBs offer large drag savings, but perform poorly when that structure breaks down off-design. Milder-performing 3D devices produce weak vortices, that may offer some boundary layer control, and SCBs also affect buffet via direct impact on shock motions and separation. To date however, design studies have largely ignored complications from the swept, spanwise-varying flows, so this thesis tackles the question of whether SCB arrays can offer useful ben
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Tirovolis, Nikolaos Labros. "Integration of commercial aircraft economic targets into the initial design process." Thesis, Imperial College London, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.425793.

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Svalstedt, Mats, and Sofia Swedberg. "Commercial Aircraft Wing Structure : - Design of a Carbon Fiber Composite Structure." Thesis, KTH, Skolan för teknikvetenskap (SCI), 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-276702.

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This project explores the classical wing structure of an commercial aircraft for an all carbon fiber reinforced polymer unmanned aerial vehicle(UAV). It is part of a collaborative work consisting of several groups researching different parts of the aircraft. The objective of this report is to present the design of the inner wing structure for a greener, more efficient scaled 2:1 version of the Skywalker X8. In order to make the aircraft as efficient as possible, the structure needs to be lightweight. The loads were first approximated using XFLR5 and a first design made. The design was then tes
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Books on the topic "Commercial Aircraft Design And Construction"

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Jackson, Scott. Systems engineering for commercial aircraft. Ashgate, 1997.

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Lomax, Ted L. Structural loads analysis for commercial transport aircraft: Theory and practice. American Institute of Aeronautics and Astronautics, 1996.

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Interiors, National Research Council (U S. ). Committee on Fire and Smoke-Resistant Materials for Commercial Aircraft. Fire- and smoke-resistant interior materials for commercial transport aircraft. National Academy Press, 1995.

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Commercial aircraft projects: Managing the development of highly complex products. Ashgate Pub., 2010.

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Gerber, Ulf. Der sowjetische Grossflugzeugbau. Elbe-Dnjepr-Verl., 2007.

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Gerber, Ulf. Der sowjetische Grossflugzeugbau. Elbe-Dnjepr-Verl., 2007.

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Gerber, Ulf. Der sowjetische Grossflugzeugbau. Elbe-Dnjepr-Verl., 2007.

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United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation. Advanced aircraft technology and Federal Aviation Administration aircraft certification: Hearing before the Subcommittee on Aviation of the Committee on Public Works and Transportation, House of Representatives, One Hundred Third Congress, first session, October 20, 1993. U.S. G.P.O., 1994.

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Aviation, United States Congress House Committee on Public Works and Transportation Subcommittee on. Advanced aircraft technology and Federal Aviation Administration aircraft certification: Hearing before the Subcommittee on Aviation of the Committee on Public Works and Transportation, House of Representatives, One Hundred Third Congress, first session, October 20, 1993. U.S. G.P.O., 1994.

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von, Vegesack Alexander, Eisenbrand Jochen, and Vitra Design Museum, eds. Airworld: Design and architecture for air travel. [The Museum], 2004.

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Book chapters on the topic "Commercial Aircraft Design And Construction"

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Breuer, Ulf Paul. "Flap Design Case Study." In Commercial Aircraft Composite Technology. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-31918-6_7.

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Breuer, Ulf Paul. "Tailored Wing Design and Panel Case Study." In Commercial Aircraft Composite Technology. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-31918-6_8.

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Wellen, Heinrich, and Peter Bartholomew. "Structural Optimisation in Aircraft Construction." In Computer Aided Optimal Design: Structural and Mechanical Systems. Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-83051-8_29.

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Jackson, Scott, and Ricardo Moraes dos Santos. "Aircraft Systems with Feedback Loops." In Systems Approach to the Design of Commercial Aircraft. CRC Press, 2020. http://dx.doi.org/10.1201/9781003053750-15.

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Mauldin, Joseph M. "Hatchery Planning, Design, and Construction." In Commercial Chicken Meat and Egg Production. Springer US, 2002. http://dx.doi.org/10.1007/978-1-4615-0811-3_36.

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Riley, Mike, and Alison Cotgrave. "Fire engineering design." In Construction Technology 2: Industrial and Commercial Building. Macmillan Education UK, 2014. http://dx.doi.org/10.1057/978-1-137-37600-8_9.

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Jackson, Scott, and Ricardo Moraes dos Santos. "Commercial Aircraft in the Context of Systems Theory." In Systems Approach to the Design of Commercial Aircraft. CRC Press, 2020. http://dx.doi.org/10.1201/9781003053750-5.

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Mistry, S., Howard Smith, and John P. Fielding. "Commercial Aircraft Design for Reduced Noise and Environmental Impact." In Variational Analysis and Aerospace Engineering. Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6_16.

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Jackson, Scott, and Ricardo Moraes dos Santos. "Vision." In Systems Approach to the Design of Commercial Aircraft. CRC Press, 2020. http://dx.doi.org/10.1201/9781003053750-1.

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Jackson, Scott, and Ricardo Moraes dos Santos. "Humans in the System." In Systems Approach to the Design of Commercial Aircraft. CRC Press, 2020. http://dx.doi.org/10.1201/9781003053750-10.

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Conference papers on the topic "Commercial Aircraft Design And Construction"

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Zhang, Xueshuang, Li Fan, Lijian Cai, and Qianwen Liu. "Study on Protection Against Large Commercial Aircraft Crash of HPR1000." In 2018 26th International Conference on Nuclear Engineering. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/icone26-81397.

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Protection against large commercial aircraft crash is a new design requirement for international advanced nuclear power plants, and gradually becomes one of important advance characteristics. The study follows the principle of balance of safety, economy, and mature achievable engineering technology, conducted by design extension condition and realistic analysis inapplicable to single failure criterion, adopts Anti-Plane Crash (APC) shell protection + redundant features physical isolation to fulfill the safety acceptance criteria, and results in the HPR1000 design scheme withdraw large commerci
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Thames, J. M., H. B. Stueber, and C. T. Vincent. "Design and Performance Features of the Marine LM1600 Gas Turbine." In ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-203.

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The GE LM1600 gas turbine is a lightweight, efficient prime mover for commercial and military marine applications. This gas turbine is a derivative of the F404 fighter jet engine whose mission objectives strongly emphasize reliability and ease of maintenance in an austere marine environment. These objectives were important to the U.S. Navy because the F/A-18 fighter jets powered by this engine are based on aircraft carriers where parts warehousing and maintenance capabilities are limited. To achieve these objectives, component designs were simplified and the total number of components was subs
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VAN BODEGRAVEN, GEORGE. "Commercial aircraft DOC methods." In Aircraft Design, Systems and Operations Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-3224.

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JACOBSON, A., and C. TSUBAKI. "Economics in new commercial aircraft design." In Aircraft Systems, Design and Technology Meeting. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2667.

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HYATT, M., R. CATON, and D. LOVELL. "Advanced materials development in commercial aircraft." In Aircraft Design and Operations Meeting. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2127.

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ADAMSON, A., and A. STUART. "Propulsion for advanced commercial transports." In Aircraft Design Systems and Operations Meeting. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-3061.

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SAGDEO, P. "Powerplants for very high capacity commercial transports." In Aircraft Design and Operations Meeting. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3131.

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WHITTENBURY, C. "A commercial view of hybrid airships." In Aircraft Systems, Design and Technology Meeting. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2703.

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HARRADINE, P., and J. QUINLIVAN. "Composites and the commercial jet - A Boeing viewpoint." In Aircraft Design and Operations Meeting. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2126.

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Yutko, Brian M., Neil Titchener, Christopher Courtin, et al. "Conceptual Design of a D8 Commercial Aircraft." In 17th AIAA Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-3590.

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Reports on the topic "Commercial Aircraft Design And Construction"

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Doyle, Jesse D., Nolan R. Hoffman, and M. Kelvin Taylor. Aircraft Arrestor System Panel Joint Improvement. U.S. Army Engineer Research and Development Center, 2021. http://dx.doi.org/10.21079/11681/41342.

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Aircraft Arresting Systems (AAS) for military applications utilize sacrificial panels made of Ultra-High Molecular Weight polyethylene (UHMWPE) that are embedded into the pavement beneath the AAS cable to protect the pavement from cable damage. Problems have been observed with the materials and practices used to seal the UHMWPE panel joints from water and debris. Data obtained from laboratory and field studies were used make improvements to current practice for sealing UHMWPE panel joints. The study evaluated four joint-sealant materials, eight alternative surface treatment and preparation tec
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