Auswahl der wissenschaftlichen Literatur zum Thema „Green aircraft design“
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Zeitschriftenartikel zum Thema "Green aircraft design"
Djojodihardjo, Harijono. „Overview of green quad bubble business jet aerodynamic configuration design“. Aircraft Engineering and Aerospace Technology 90, Nr. 3 (09.04.2018): 566–82. http://dx.doi.org/10.1108/aeat-12-2016-0241.
Der volle Inhalt der QuelleBrooker, P. „Civil aircraft design priorities: air quality? climate change? noise?“ Aeronautical Journal 110, Nr. 1110 (August 2006): 517–32. http://dx.doi.org/10.1017/s0001924000001408.
Der volle Inhalt der QuelleXi, Mingze. „Rational Design of Future Potential Electric Aircraft“. Journal of Physics: Conference Series 2434, Nr. 1 (01.01.2023): 012006. http://dx.doi.org/10.1088/1742-6596/2434/1/012006.
Der volle Inhalt der QuelleBooker, Julian, Caius Patel und Phillip Mellor. „Modelling Green VTOL Concept Designs for Reliability and Efficiency“. Designs 5, Nr. 4 (28.10.2021): 68. http://dx.doi.org/10.3390/designs5040068.
Der volle Inhalt der QuelleKeivanpour, Samira, Daoud Ait Kadi und Christian Mascle. „End of life aircrafts recovery and green supply chain (a conceptual framework for addressing opportunities and challenges)“. Management Research Review 38, Nr. 10 (19.10.2015): 1098–124. http://dx.doi.org/10.1108/mrr-11-2014-0267.
Der volle Inhalt der QuelleBaalbergen, Erik, Wim Lammen, Nikita Noskov, Pier-Davide Ciampa und Erwin Moerland. „Integrated collaboration capabilities for competitive aircraft design“. MATEC Web of Conferences 233 (2018): 00015. http://dx.doi.org/10.1051/matecconf/201823300015.
Der volle Inhalt der QuelleKernstine, Kemp, Bryan Boling, Latessa Bortner, Eric Hendricks und Dimitri Mavris. „Designing for a Green Future: A Unified Aircraft Design Methodology“. Journal of Aircraft 47, Nr. 5 (September 2010): 1789–97. http://dx.doi.org/10.2514/1.c000239.
Der volle Inhalt der QuelleFera, Marcello, Raffaele Abbate, Mario Caterino, Pasquale Manco, Roberto Macchiaroli und Marta Rinaldi. „Economic and Environmental Sustainability for Aircrafts Service Life“. Sustainability 12, Nr. 23 (03.12.2020): 10120. http://dx.doi.org/10.3390/su122310120.
Der volle Inhalt der QuelleOuyang, Zeyu, Theoklis Nikolaidis und Soheil Jafari. „Integrated Power and Thermal Management Systems for Civil Aircraft: Review, Challenges, and Future Opportunities“. Applied Sciences 14, Nr. 9 (26.04.2024): 3689. http://dx.doi.org/10.3390/app14093689.
Der volle Inhalt der QuelleWang, Yu, Wenyuan Ma und Zhaolin Chen. „Sensitivity Analysis for Design Parameters of Electric Tilt-Rotor Aircraft“. Aerospace 11, Nr. 4 (20.04.2024): 322. http://dx.doi.org/10.3390/aerospace11040322.
Der volle Inhalt der QuelleDissertationen zum Thema "Green aircraft design"
Saves, Paul. „High dimensional multidisciplinary design optimization for eco-design aircraft“. Electronic Thesis or Diss., Toulouse, ISAE, 2024. http://www.theses.fr/2024ESAE0002.
Der volle Inhalt der QuelleNowadays, there has been significant and growing interest in improving the efficiency of vehicle design processes through the development of tools and techniques in the field of multidisciplinary design optimization (MDO). In fact, when optimizing both the aerodynamics and structures, one needs to consider the effect of the aerodynamic shape variables and structural sizing variables on the weight which also affects the fuel consumption. MDO arises as a powerful tool that can perform this trade-off automatically. The objective of the Ph. D project is to propose an efficient approach for solving an aero-structural wing optimization process at the conceptual design level. The latter is formulated as a constrained optimization problem that involves a large number of design variables (typically 700 variables). The targeted optimization approach is based on a sequential enrichment (typically efficient global optimization (EGO)), using an adaptive surrogate model. Kriging surrogate models are one of the most widely used in engineering problems to substitute time-consuming high fidelity models. EGO is a heuristic method, designed for the solution of global optimization problems that has performed well in terms of quality of the solution computed. However, like any other method for global optimization, EGO suffers from the curse of dimensionality, meaning that its performance is satisfactory on lower dimensional problems, but deteriorates as the dimensionality of the optimization search space increases. For realistic aircraft wing design problems, the typical size of the design variables exceeds 700 and, thus, trying to solve directly the problems using EGO is ruled out. In practical test cases, high dimensional MDO problems may possess a lower intrinsic dimensionality, which can be exploited for optimization. In this context, a feature mapping can then be used to map the original high dimensional design variable onto a sufficiently small design space. Most of the existing approaches in the literature use random linear mapping to reduce the dimension, sometimes active learning is used to build this linear embedding. Generalizations to non-linear subspaces are also proposed using the so-called variational autoencoder. For instance, a composition of Gaussian processes (GP), referred as deep GP, can be very useful. In this PhD thesis, we will investigate efficient parameterization tools to significantly reduce the number of design variables by using active learning technics. An extension of the method could be also proposed to handle mixed continuous and categorical inputs using some previous works on low dimensional problems. Practical implementations within the OpenMDAO framework (an open source MDO framework developed by NASA) are expected
Pecorella, Daniele. „Methodology for the design and optimization of a morphing wing droop-nose structure for greener aircraft“. Master's thesis, Alma Mater Studiorum - Università di Bologna, 2022.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Green aircraft design"
Quagliarella, Domenico, Elisa Morales Tirado und Andrea Bornaccioni. „Risk Measures Applied to Robust Aerodynamic Shape Design Optimization“. In Flexible Engineering Toward Green Aircraft, 153–68. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-36514-1_9.
Der volle Inhalt der QuelleIlg, R. „Systematic approach of upscaling aircraft parts and sub-modules to aircraft level“. In Green Design, Materials and Manufacturing Processes, 289–92. CRC Press, 2013. http://dx.doi.org/10.1201/b15002-56.
Der volle Inhalt der Quelle„Airline Effective Noise Management Strategies“. In Airline Green Operations Strategies, 131–52. IGI Global, 2020. http://dx.doi.org/10.4018/978-1-7998-4255-2.ch006.
Der volle Inhalt der QuelleSuder, Kenneth L., und James D. Heidmann. „Improvement of aeropropulsion fuel efficiency through engine design“. In Green Aviation: Reduction of Environmental Impact Through Aircraft Technology and Alternative Fuels, 49–79. CRC Press, 2018. http://dx.doi.org/10.1201/b20287-4.
Der volle Inhalt der QuelleLewis, Kristin C., Dan F. B. Flynn und Jeffrey J. Steiner. „Biofuel feedstocks and supply chains: how ecological models can assist with design and scaleup“. In Green Aviation: Reduction of Environmental Impact Through Aircraft Technology and Alternative Fuels, 247–68. CRC Press, 2018. http://dx.doi.org/10.1201/b20287-12.
Der volle Inhalt der QuelleAshwini, A., S. R. Sriram, A. Manisha und J. Manoj Prabhakar. „Artificial Intelligence's Impact on Thrust Manufacturing With Innovations and Advancements in Aerospace“. In Industry Applications of Thrust Manufacturing, 197–220. IGI Global, 2024. http://dx.doi.org/10.4018/979-8-3693-4276-3.ch008.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Green aircraft design"
Pustina, L. „Towards multidisciplinary design optimization of next-generation green aircraft“. In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-97.
Der volle Inhalt der QuelleCollier, Fayette, und Richard Wahls. „Aerodynamic Design and Enabling Technologies for Green Aircraft (Invited)“. In 27th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-4315.
Der volle Inhalt der QuelleIsmail, M. S., M. F. Mohammed, K. N. Sivaraman, S. N. Sivaraman und M. I. Hussain. „Smart IoT temperature and humidity alert system at aircraft composite storage area“. In PROCEEDINGS OF GREEN DESIGN AND MANUFACTURE 2020. AIP Publishing, 2021. http://dx.doi.org/10.1063/5.0044198.
Der volle Inhalt der QuelleWerner-Westphal, Christian, Wolfgang Heinze und Peter Horst. „Multidisciplinary Integrated Preliminary Design Applied to Future Green Aircraft Configurations“. In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-655.
Der volle Inhalt der QuelleChen, G., W. Deng und J. Zhang. „Design and research of green electric taxiing system based on MBSE method“. In CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020). Institution of Engineering and Technology, 2021. http://dx.doi.org/10.1049/icp.2021.0352.
Der volle Inhalt der QuelleLandrum, D. Brian, Kyle Schikore und Ryan Longchamps. „Design and Flight Testing of an Experimental Aircraft for Green Leveraged Energy“. In 55th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-0514.
Der volle Inhalt der QuelleDimino, Ignazio, Salvatore Ameduri und Antonio Concilio. „Preliminary Failure Analysis and Structural Design of a Morphing Winglet for Green Regional Aircraft“. In ASME 2018 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/smasis2018-8236.
Der volle Inhalt der QuelleKoster, Jean, Ewald Kraemer, Claus-Dieter Munz, Dries Verstraete, K. C. Wong und Alec Velazco. „Workforce Development for Global Aircraft Design“. In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-62273.
Der volle Inhalt der QuelleKoster, Jean, Scott Balaban, Derek Hillery, Cody Humbargar, Derek Nasso, Eric Serani und Alec Velazco. „Design of a Blended Wing Body UAS With Hybrid Propulsion“. In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-62126.
Der volle Inhalt der QuellePallavi, M., Pramod Kumar, Tanweer Ali, Satish B. Shenoy und Lokesh Sharma. „Design and Analysis of Patch Antenna with T-Shape DGS for Aircraft Surveillance Applications“. In 2022 6th International Conference on Green Technology and Sustainable Development (GTSD). IEEE, 2022. http://dx.doi.org/10.1109/gtsd54989.2022.9989196.
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