Relevant bibliographies by topics / Aeronautic engineering

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Aeronautic engineering'

Author: Grafiati
Published: 30 May 2022
Last updated: 31 July 2025

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Journal articles on the topic "Aeronautic engineering"

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Zhao, Yan Ling, Chun Yu Che, Hong Bo Wang, Zi Yan Yun, and Guan Hong Xu. "Application of Knowledge Based Engineering in Aeronautics Mold Parts Parametric Design." Advanced Materials Research 765-767 (September 2013): 47–50. http://dx.doi.org/10.4028/www.scientific.net/amr.765-767.47.

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In the process of designing aeronautic composite mold parts, previous designing knowledge and expertise cant be well used, the cycle of parts modeling is long and its production efficiency is low. According to the classification and characteristics of aeronautic mold parts and the knowledge engineering technology, based on the fusion module in UG6.0, we establish its repository by the knowledge acquisition, knowledge representation and knowledge reasoning of aeronautic mold parts. With the UG secondary development tools, UG/Open Menuscript and UG/Open Uistyler, we develop user menu and paramet
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Qian, Hao Han, Yuan Ming Ding, and Jia Cheng. "Research in Thermo-Physical Property Testing System of Aeronautic PMMA Based on Temperature-Pressure Parameters." Advanced Materials Research 647 (January 2013): 828–32. http://dx.doi.org/10.4028/www.scientific.net/amr.647.828.

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Because of the differences in physical properties, the aeronautic PMMA for porthole may easily craze, crack and even explode in flight. In this paper, the operating conditions for porthole were analyzed and testing methods of PMMA’s thermo-physical properties were studied considering the two main factors, temperature and pressure, which affects porthole’s operating life. At last a thermo-physical property testing system of aeronautic PMMA based on temperature-pressure parameters was designed. This device could preferably simulate the operating conditions and conduct continuous fatigue test for
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Brito-Acuña, Guillermo. "Aeronautic maturity cybersecurity: a framework." DYNA 90, no. 227 (2023): 24–34. http://dx.doi.org/10.15446/dyna.v90n227.107420.

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This article presents the results of a systematic review of the methods to implement cybersecurity maturity. Based on them, it proposes a framework for excellence in aeronautical cybersecurity that integrates the objectives of aeronautical cybersecurity with capabilities and requirements, which contributes to increasing the maturity of aeronautical cybersecurity. It exposes 13 objectives with 120 capabilities and 5 functional maturity levels to gradually meet up to 600 aeronautical cybersecurity requirements. Which were taken from articles with good practices associated with publications of th
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Boulos, Federico, Georg Frederik Riemschneider, and Stefano Caizzone. "3D Phased Array Enabling Extended Field of View in Mobile Satcom Applications." Electronics 13, no. 2 (2024): 310. http://dx.doi.org/10.3390/electronics13020310.

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Satellite communication (satcom) is experiencing increased interest to cover the connectivity gaps of terrestrial networks. To ensure high performance and throughput for the user—and even more so in Communications-On-The-Move(COTM) systems, e.g., in aeronautics—steerable antennas such as phased arrays are required to adjust the beam so as to follow the satellite’s trajectory. The mutual movement of terminals and satellite in COTM systems calls for a broad Field of View (FoV) and, hence, poses a challenge to common planar systems. For improving the FoV, common solutions require ad hoc designs,
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Deque, R., and P. Bachelier. "Future aeronautic environment FMS/ATC/Pilot." Aeronautical Journal 94, no. 940 (1990): 341–43. http://dx.doi.org/10.1017/s0001924000023290.

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Abstract The scope of the air-ground data links, which have been developed over the last ten years to meet the airlines' operational requirements, will be extended in future years.Air traffic control is one of the fields which will certainly make extensive use of this type of link. Indeed, it appears to be necessary to deal with the problem of traffic saturation globally by taking account of the navigation capabilities of modern aircraft as regards precision and the considerable automated flight/ground exchange possibilities which will be provided by future telecommunication networks.The conte
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Tommasino, Domenico, Federico Moro, Bruno Bernay, Thibault De Lumley Woodyear, Enrique de Pablo Corona, and Alberto Doria. "Vibration Energy Harvesting by Means of Piezoelectric Patches: Application to Aircrafts." Sensors 22, no. 1 (2022): 363. http://dx.doi.org/10.3390/s22010363.

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Vibration energy harvesters in industrial applications usually take the form of cantilever oscillators covered by a layer of piezoelectric material and exploit the resonance phenomenon to improve the generated power. In many aeronautical applications, the installation of cantilever harvesters is not possible owing to the lack of room and/or safety and durability requirements. In these cases, strain piezoelectric harvesters can be adopted, which directly exploit the strain of a vibrating aeronautic component. In this research, a mathematical model of a vibrating slat is developed with the modal
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Füchter, Simone Keller, Mário Sérgio Schlichting, and George Salazar. "Aeronautic pilot training and augmented reality." ACTA IMEKO 10, no. 3 (2021): 66. http://dx.doi.org/10.21014/acta_imeko.v10i3.1038.

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<p class="Abstract">A pre-flight checklist requires in-depth technical knowledge of the aircraft and its dashboard, avionics, instruments, functions, and cabin layout. The student in training to be a pilot or advanced pilot, to obtain an updated certification, must know very thoroughly each instrument and its position on the flight panel. Every second spent searching for the location of an instrument, switch or indicator can waste time, resulting in a poor start-up procedure and possibly a safety hazard. The objective of this research was to obtain preliminary data to determine if the us
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González Ojeda, Itzel De Jesús, Pablo Bengoa, Aitor Ibarguren, et al. "Robot Coordination: Aeronautic Use Cases Handling Large Parts." Designs 6, no. 6 (2022): 116. http://dx.doi.org/10.3390/designs6060116.

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The coordination of two collaborative robots to handle and hold huge parts is the main topic of this research. This study shows how flexible systems may accommodate large-volume components while situating components with a displacement precision between robots of no more than 10 mm into the parts, with the assistance of a single operator. The robots must be able to keep the parts in place while coordinating their movements to handle the parts and reducing external stressors. This paper suggests using collaborative robots to integrate flexible tools for adaptability to various elements in order
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Xia, Qianshan, Zhichun Zhang, Yanju Liu, and Jinsong Leng. "Buckypaper and its composites for aeronautic applications." Composites Part B: Engineering 199 (October 2020): 108231. http://dx.doi.org/10.1016/j.compositesb.2020.108231.

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Vietri, U., L. Guadagno, M. Raimondo, L. Vertuccio, and K. Lafdi. "Nanofilled epoxy adhesive for structural aeronautic materials." Composites Part B: Engineering 61 (May 2014): 73–83. http://dx.doi.org/10.1016/j.compositesb.2014.01.032.

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Dissertations / Theses on the topic "Aeronautic engineering"

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Philippe, Alexis. "Optimisation of an aeronautic production line through the managementof tools and the shortage of items." Thesis, KTH, Flygdynamik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-261701.

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This thesis work is part of a process to ensure the production ramp-up of the A320neo aircraft pylons at Airbus Saint-Eloi factory (Toulouse). The aim of the project was to optimise the production management in order to sustain the transition to a serial production of the assembly lines. The objective of the thesis work was to develop a model to prevent the downtime of the production lines caused by the shortage of the assembly lines or the unavailability of tools on workstations.Firstly, the work investigates the existing models in order to understand the causes of stocks variability. Perform
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Ivliev. "SPACE X’S ROCKET CONCEPTS – STEP FORWARD IN AERONAUTICAL ENGINEERING." Thesis, Київ 2018, 2018. http://er.nau.edu.ua/handle/NAU/33718.

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Alroqi, Abdurrhman Atig. "Investigation of the heat and wear of aircraft landing gear tyres." Thesis, University of Sussex, 2017. http://sro.sussex.ac.uk/id/eprint/68761/.

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In aircraft, the main landing gear wheels skid on the runway at the moment of touchdown because of high slip. A slipping tyre generates enough heat to melt its rubber. Melted rubber is easily eroded by the friction force between the tyre and runway; and part of eroded rubber stays on the runway, and other is burnt off as smoke. Since the early days of airplane use, a number of ideas have been patented to improve tyre safety and decrease the substantial wear and smoke during every landing by spinning the gear wheels before touchdown. In this thesis, there are three parts of research work. First
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Alkandri, Ahmad. "Design and performance assessment of correlation filters for the detection of objects in high clutter thermal imagery." Thesis, University of Sussex, 2014. http://sro.sussex.ac.uk/id/eprint/49954/.

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The research reported in this thesis has examined means of enhancing the performance of the Optimal Trade-off Maximum Average Correlation Height (OT-MACH) filter for target detection in Forward Looking Infra-Red (FLIR) imagery acquired from a helicopter and border security FLIR camera in northern Kuwait. The data acquired with these FLIR sensors allows real-world evaluation of the comparative performance of the various filters that have been developed in the thesis. The results obtained have been quantified using well known performance measures such as Peak to Side-lobe Ratio (PSR) and Total D
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Bramer, Elinor C. "Development of a particle in cell code for the simulation of dual stage ion thrusters." Thesis, University of Sussex, 2014. http://sro.sussex.ac.uk/id/eprint/48913/.

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This thesis focuses on the design, development and testing of a two dimensional particle in cell (PIC) code (PICSIE) written in Matlab. The code is applied to the specific problem of modelling the performance of dual stage ion thrusters. The code simulates one full aperture within dual stage ion thruster systems, focusing on the flow of ions through the aperture. Only the ions have been included in the simulation in order to minimize running time. The results produced by the simulation code are compared with results obtained from the vacuum chamber testing of the DS4G prototype, along with res
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Langari, Mostafa. "Large eddy simulation of separated boundary layer transition under free-stream turbulence." Thesis, University of Sussex, 2014. http://sro.sussex.ac.uk/id/eprint/48940/.

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Physics of laminar-to-turbulent transition in a separated-reattached flow subjected to two free-stream turbulence levels have been explored using Large-Eddy Simulation (LES). Separation of the laminar boundary layer occurs at a curvature change over a flat plate with a semi-circular leading edge. A numerical trip has been used to generate the targeted free-stream turbulence levels. A dynamic Sub-grid-scale (SGS) model has been employed and excellent agreement has been achieved between the LES results and the experimental data. Detailed investigation of the LES data has been carried out to expl
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Біла, Світлана Олексіївна, and Svitlana Bila. "Strategic priorities of aviation services market’s competitiveness growth in Ukraine within globalization." Thesis, National Aviation University, 2016. http://er.nau.edu.ua/handle/NAU/38534.

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The basic strategic priorities of aviation services market’s competiveness growth in Ukraine within globalization terms are defined in the article. The special attention is given to the prospects of improving, security and achieving correspondence of national aviation services market’s standards with international ones under the terms of Ukraine’s joining Common aviation space with EU and rules of ‘common aviation area’. The main priorities of aviation branch in Ukraine are defined concerning its competitiveness growth.
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Stringfellow, Margaret Virgina. "Safety-driven system engineering process." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/49685.

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Thesis (S. M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.<br>MIT Barker Library copy: leaves 82 to 106 bound upside-down.<br>Includes bibliographical references (leaves 56-59).<br>As the demand for high-performing complex systems has increased, the ability of engineers to meet that demand has not kept pace. The creators of the traditional system engineering processes did not anticipate modern complex systems, and the application of traditional processes to complex systems such as spacecraft has repeatedly led to disastrous results. Too often, system sa
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Guiho, Audren. "Design, development and use of a mechanism simulator for aeronautical engineering." Thesis, KTH, Flygdynamik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-244830.

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This paper deals with the strategy for developing a very specific mechanism simulator. This mechanism is currently designed by Safran Group. A previous version of the same mechanism does exist but the scale is not on a like-for-like basis. Therefore, physical phenomena involved in this mechanism and their magnitude are not comparable to the previous version of the mechanism and this is why a new simulator has been developed (specified, coded and validated) from scratch. The paper addresses the strategy adopted for modelling a mechanism laying on a wide set of parameters as well as its use.<br>
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Coffee, Thomas Merritt. "A modular programming language for engineering design." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43080.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.<br>Includes bibliographical references (p. 137-142).<br>We introduce a new universal model of computation called MDPL that generalizes other functional models like the lambda calculus and combinatory logic. This model leads naturally to a new type of programming language that combines the key strengths of imperative and functional languages for development and analysis of programs. These strengths have particular relevance for rapid analysis of large-scale engineering design problems. MDPL uses a
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Books on the topic "Aeronautic engineering"

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Eastburg, Steven R. An engineering study of altitude determination deficiencies of the Service Aircraft Instrumentation Package (SAIP). Naval Postgraduate School, 1991.

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Research, Institute for Career. Careers in aerospace engineering: Aeronautics - astronautics. Institute for Career Research, 2003.

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Laudański, Ludomir M. Computational probability for aeronautical engineering. Institute of Aviation Scientific Library, 2002.

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United States. National Aeronautics and Space Administration. NASA thesaurus aeronautics vocabulary. NASA, 1991.

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1923-, Pelegrin Marc, and Hollister Walter M. 1930-, eds. Concise encyclopedia of aeronautics & space systems. Pergamon Press, 1993.

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Bi︠u︡shgens, G. S. Opirai︠a︡sʹ na silu razuma: Vospominanii︠a︡ i razmyshlenii︠a︡ o razvitii otechestvennoĭ aviat︠s︡ii. Nauka, 2012.

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Rodionov, B. I. Avianost︠s︡y: Istorii︠a︡ i perspektivy. Voen. izd-vo, 2004.

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Alpatov, I. M. Zhivai︠a︡ pami︠a︡tʹ o vremeni i o sebe: Vnutri aviat︠s︡ii i kosmonavtiki. Ladoga-100, 2005.

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Burke, Mary V. Profiles--aeronautical/astronautical engineering: Human resources and funding. National Science Foundation, 1989.

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Burke, Mary V. Profiles--aeronautical/astronautical engineering: Human resources and funding. National Science Foundation, 1989.

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Book chapters on the topic "Aeronautic engineering"

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Briand, William, Marc Rébillat, Mikhail Guskov, and Nazih Mechbal. "Damage Imaging Post Processing for Delamination Size Assessment of CFRP Aeronautic Structures." In Lecture Notes in Civil Engineering. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-64594-6_15.

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Rocha, Luis, Paul Bills, Michael Marxer, and Enrico Savio. "Training in the Aeronautic Industry for Geometrical Quality Control and Large Scale Metrology." In Lecture Notes in Mechanical Engineering. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-18177-2_16.

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Zhou, Guoqiang, Jiuqin Liu, and Xiao Liu. "Remaining Useful Life Prediction of Key Aeronautic Equipment Based on Improved LSTM Autoencoder." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-9765-3_34.

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Dimino, I., and V. Quaranta. "A Wavelet-Based System for Structural Health Monitoring of Aeronautic Structures." In Experimental Analysis of Nano and Engineering Materials and Structures. Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6239-1_225.

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Koujalagi, B. G., Ramesh Katti, R. N. Chikkanagoudar, Nagaraj Kishor Kelageri, R. G. Lingannavar, and Zeeshan Ali. "Methods and Materials for Metal Additive Manufacturing: A Critical Review on Aeronautic and Aerospace Sectors." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-4324-7_25.

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Chen, Hang-hang, and Li-xin Pan. "Study on the Strategies of Target Cost Management in the Supply Chain of Aeronautic Complex Product." In Proceedings of the 22nd International Conference on Industrial Engineering and Engineering Management 2015. Atlantis Press, 2016. http://dx.doi.org/10.2991/978-94-6239-177-2_51.

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Di Palma, Paola, Saverio De Vito, Mara Miglietta, et al. "E-Nose as a Potential Quality Assurance Technology for the Detection of Surface Contamination by Aeronautic Fluids." In Lecture Notes in Electrical Engineering. Springer International Publishing, 2013. http://dx.doi.org/10.1007/978-3-319-00684-0_85.

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Amri, Rihem, Adnen Laamouri, and Raouf Fathallah. "Prediction of Water Jet Peening Effects on Surface Integrity and High Cycle Fatigue Behavior of Al 7075-T6 Aeronautic Aluminum Alloy." In Lecture Notes in Mechanical Engineering. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-70428-4_8.

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Paroissien, Eric, Marc Sartor, and Jacques Huet. "Hybrid (Bolted/Bonded) Joints Applied to Aeronautic Parts: Analytical One-Dimensional Models of a Single-Lap Joint." In Advances in Integrated Design and Manufacturing in Mechanical Engineering II. Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6761-7_7.

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Jafer, Shafagh, Umut Durak, Hakan Aydemir, Richard Ruff, and Thorsten Pawletta. "Advances in Software Engineering and Aeronautics." In Advances in Aeronautical Informatics. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-75058-3_7.

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Conference papers on the topic "Aeronautic engineering"

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Girondin, Victor, and Stephane Morel. "Control Engineering Approach in Safety Management Systems." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12212.

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Safety Management Systems (SMS) are mainly based on an operational feedback approach for continuous safety enhancement. Closed loop approaches have been dramatically developed and applied in aeronautics by control engineers. In this article, SMS is redefined in terms of automatic control and this analogy leads to the identification of three classical feedback strategies. The theoretical effect of these strategies on performances is also discussed. As in any closed loop systems, the importance of understanding how the mission stakeholders react will be found to be particularly crucial. The last
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Ramirez Garcia, Alison Celeste, Sergio Guillermo Torres Cedillo, and Rodrigo Florencio da Silva. "FORMATION IN AERONAUTICAL ENGINEERING: NON-INVASIVE BALANCING METHODS FOR ENGINES." In 17th annual International Conference of Education, Research and Innovation. IATED, 2024. https://doi.org/10.21125/iceri.2024.1357.

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Quadrini, Fabrizio, Denise Bellisario, Leandro Iorio, Alice Proietti, Nicola Gallo, and Loredana Santo. "Autoclave Molding of Carbon Fiber Laminates With Interlaminar Carbon Nanotubes." In ASME 2022 17th International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/msec2022-85480.

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Abstract Carbon nanotubes (CNTs) are deposited between prepreg plies of a carbon fiber reinforced (CFR) laminate during lamination to improve laminate strength. An easy manufacturing procedure has been implemented for this aim in laboratory. CNTs are diluted in a solvent, and subsequently sprayed on commercial woven fabric prepregs for aeronautics. Solvent evacuation is carried out at room temperature. Final composite laminates are produced by vacuum bagging and autoclave molding of coated prepreg plies, by following the typical industrial procedure of aeronautic parts. Quasi-isotropic square
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Guimarães Ono, Nicolas, Lucas Antunes, Giovanna Scala, Caio Ribeiro, and Bruno Chieregatti. "A CFD Analysis of a Morphing Wing for Aeronautic Applications." In 26th International Congress of Mechanical Engineering. ABCM, 2021. http://dx.doi.org/10.26678/abcm.cobem2021.cob2021-0535.

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Tourneroche, Paul, Jean-Claude Gelin, Thierry Barrière, and Mohamed Sahli. "Development and Characterization of Inconel-Based Mixtures for Metal Injection Molding Applications." In ASME 2015 International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/msec2015-9359.

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In this paper, the development of a new mixture, called feedstock, based on nickel super-alloys for Metal Injection Molding (MIM) is presented. This feedstock, which will be used to obtain metallic parts for the aeronautic industry, is a mixture of the appropriate, environmentally friendly polymers and metallic powders. Many scientific problems should be taken into account. For example, it requires tight control of the process to achieve the strict chemical and physical properties, because of the application in aeronautic industry. Another difficulty is the large dimension and functional requi
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Qin Ming, Dong Lei, Huang Xiaojiang, and Liao Xiaozhong. "A rapid design method for high speed aeronautic switched reluctance generator." In 2011 International Conference on Electric Information and Control Engineering (ICEICE). IEEE, 2011. http://dx.doi.org/10.1109/iceice.2011.5777095.

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Wang, Hong, and Xiaojie Lv. "Implementation of Data Warehouse at Domestic Large Aeronautic Hub for Flight Information." In 2009 International Conference on Computational Intelligence and Software Engineering. IEEE, 2009. http://dx.doi.org/10.1109/cise.2009.5366924.

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Gough, Kerry M., and Nipa Phojanamongkolkij. "Employing Model-Based Systems Engineering (MBSE) on a NASA Aeronautic Research Project: A Case Study." In 2018 Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-3361.

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Valente, M. "How space technologies can address the impact of climate change on aeronautic and the aviation." In Aerospace Science and Engineering. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902677-36.

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Abstract. Aviation and flight management are strictly influenced by environmental conditions. Greater variability of the climate and the atmospheric phenomena carries greater risks for air navigation and increase cancellations and delay. An increase in the frequency and intensity of storms, torrential rains, hailstorms, fog, wind gusts, and other meteorological events may lead to a reduction in flight times and from a design point of view an increase in the weight of the aircraft, to counteract higher loads in operation. All of this could produce rising management and operational costs, as wel
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Rabalo, M. A., Amabel Garcia-Dominguez, Eva María Rubio, Marta María Marín, and Beatriz de Agustina. "Last Trends in the Application of the Hybrid Additive and Subtractive Manufacturing in the Aeronautic Industry." In 10th Manufacturing Engineering Society International Conference. Trans Tech Publications Ltd, 2023. http://dx.doi.org/10.4028/p-m9diuh.

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In recent years, hybrid additive and subtractive manufacturing has made its way as a new approach to manufacturing complex parts, with high added value and high requirements, imposed by the leading sectors of the industry, among which the aeronautical industry stands out. This still novel concept combines the additive manufacturing ability to generate parts with complex geometry and the great dimensional, geometric, and surface quality that allows the already mature subtractive manufacturing, and it does so by surpassing the concept of post-processing machining. Thus, the integration of both f
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Reports on the topic "Aeronautic engineering"

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Haas, David J., Eric J. Silberg, and Judah H. Milgram. Birth of U.S. Naval Aeronautical Engineering and Phenomenal Rise to Excellence. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada558168.

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Bidier, S., U. Khristenko, R. Tosi, R. Rossi, and C. Soriano. D7.3 Report on UQ results and overall user experience. Scipedia, 2021. http://dx.doi.org/10.23967/exaqute.2021.9.002.

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This deliverable report focuses on the main Uncertainty Quanti cation (UQ) results obtained within the EXAscale Quanti cation of Uncertainties for Technology and Science Simulation (ExaQUte) project. Details on the turbulent wind inlet generator, that enables the supply of random, yet steady, wind velocity boundary conditions during run-time, are given in section 2. This enables the developed UQ workflow, whose results are presented on the basis of the Commonwealth Advisory Aeronautical Council (CAARC) as described in Deliverable 7.1. Finally, the completed UQ workflow and the results are eval
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Platzer, Max F., and Raymond P. Shreeve. Summary of Research 2001, Department of Aeronautics and Astronautics, Graduate School of Engineering and Applied Sciences. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada415406.

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Silberg, Eric J., and David J. Haas. Developing the Navy's NC Flying Boats: Transforming Aeronautical Engineering for the First Transatlantic Flight. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada558169.

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Pisani, William, Dane Wedgeworth, Michael Roth, John Newman, and Manoj Shukla. Exploration of two polymer nanocomposite structure-property relationships facilitated by molecular dynamics simulation and multiscale modeling. Engineer Research and Development Center (U.S.), 2023. http://dx.doi.org/10.21079/11681/46713.

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Abstract:
Polyamide 6 (PA6) is a semi-crystalline thermoplastic used in many engineering applications due to good strength, stiffness, mechanical damping, wear/abrasion resistance, and excellent performance-to-cost ratio. In this report, two structure-property relationships were explored. First, carbon nanotubes (CNT) and graphene (G) were used as reinforcement molecules in simulated and experimentally prepared PA6 matrices to improve the overall mechanical properties. Molecular dynamics (MD) simulations with INTERFACE and reactive INTERFACE force fields (IFF and IFF-R) were used to predict bulk and You
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