Статті в журналах з теми "Stiffened Composite Wing"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся з топ-50 статей у журналах для дослідження на тему "Stiffened Composite Wing".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Переглядайте статті в журналах для різних дисциплін та оформлюйте правильно вашу бібліографію.
Sahadevan, Vijay, Yoann Bonnefon, and Tim Edwards. "A Meta-Heuristic Based Weight Optimisation for Composite Wing Structural Analysis." Applied Mechanics and Materials 5-6 (October 2006): 305–14. http://dx.doi.org/10.4028/www.scientific.net/amm.5-6.305.
Повний текст джерелаButler, R. "Optimum design of composite stiffened wing panels — a parametric study." Aeronautical Journal 99, no. 985 (May 1995): 169–77. http://dx.doi.org/10.1017/s0001924000028335.
Повний текст джерелаLiu, Tie Jun, Yong Zhang, Gang Li, and Feng Hui Wang. "Dynamic Response Analysis for the Solar-Powered Aircraft Composite Wing Panel with Viscoelastic Damping Layer." Applied Mechanics and Materials 105-107 (September 2011): 491–94. http://dx.doi.org/10.4028/www.scientific.net/amm.105-107.491.
Повний текст джерелаHwu, Chyanbin, and Z. S. Tsai. "Aeroelastic Divergence of Stiffened Composite Multicell Wing Structures." Journal of Aircraft 39, no. 2 (March 2002): 242–51. http://dx.doi.org/10.2514/2.2945.
Повний текст джерелаBhowmik, Krishnendu, Shamim Akhtar, Raj Kumar Kalshyan, Niloy Khutia, and Amit Roy Choudhury. "CNT Reinforced Laminated Composite under In-Plane Tensile Loading: A Finite Element Study." Materials Science Forum 978 (February 2020): 323–29. http://dx.doi.org/10.4028/www.scientific.net/msf.978.323.
Повний текст джерелаKATO, Yoko, Ning HU, Masaki KAMEYAMA, and Hisao FUKUNAGA. "Optimum Design of Composite Wing Considering Stiffened Panel Buckling." Proceedings of Conference of Tohoku Branch 2002.37 (2002): 208–9. http://dx.doi.org/10.1299/jsmeth.2002.37.208.
Повний текст джерелаKATO, Yoko, Masaki KAMEYAMA, Ning HU, and Hisao FUKUNAGA. "Optimum Design of Composite Wing Considering Stiffened Panel Buckling." Transactions of the Japan Society of Mechanical Engineers Series A 70, no. 691 (2004): 479–86. http://dx.doi.org/10.1299/kikaia.70.479.
Повний текст джерелаYang, Xue-Yong, and Jun Xiao. "Research Progress on Analytical and Numerical Prediction of Curing Deformation in Thermoset for Large Composite Parts." Science of Advanced Materials 14, no. 4 (April 1, 2022): 669–81. http://dx.doi.org/10.1166/sam.2022.4247.
Повний текст джерелаRomano, Fulvio, Monica Ciminello, Assunta Sorrentino, and Umberto Mercurio. "Application of structural health monitoring techniques to composite wing panels." Journal of Composite Materials 53, no. 25 (April 10, 2019): 3515–33. http://dx.doi.org/10.1177/0021998319843333.
Повний текст джерелаDe Angelis, Giovanni, Michele Meo, D. P. Almond, S. G. Pickering, and U. Polimeno. "Impact Damage Detection in a Stiffened Composite Wing Panel Using Digital Shearography and Thermosonics." Key Engineering Materials 471-472 (February 2011): 904–9. http://dx.doi.org/10.4028/www.scientific.net/kem.471-472.904.
Повний текст джерелаKumar, K. C. Nithin, Gopal Gupta, Saurabh Lakhera, and Amir Shaikh. "Structural Optimization of Composite Stiffened Panel of a Transport Aircraft Wing using CAE Tools." Materials Today: Proceedings 2, no. 4-5 (2015): 2588–94. http://dx.doi.org/10.1016/j.matpr.2015.07.213.
Повний текст джерелаWiggenraad, J. F. M., X. Zhang, and G. A. O. Davies. "Impact damage prediction and failure analysis of heavily loaded, blade-stiffened composite wing panels." Composite Structures 45, no. 2 (June 1999): 81–103. http://dx.doi.org/10.1016/s0263-8223(98)00132-9.
Повний текст джерелаK.C., Nithin Kumar, Subhash Chavadaki, Amir Shaikh, Durgeshwar Pratap Singh, and Shwetank Avikal. "Weight optimization of a hat stiffened panel of a typical transport aircraft composite wing." Materials Today: Proceedings 26 (2020): 471–74. http://dx.doi.org/10.1016/j.matpr.2019.12.087.
Повний текст джерелаSkrna-Jakl, I. C., M. A. Stiftinger, and F. G. Rammerstorfer. "Numerical investigations of an imperfect stringer-stiffened composite wing torsion box—an analysis concept." Composites Part B: Engineering 27, no. 1 (January 1996): 59–69. http://dx.doi.org/10.1016/1359-8368(95)00007-0.
Повний текст джерелаdos Santos, Rogério Rodrigues, Tulio Gomes de Paula Machado, and Saullo Giovani Pereira Castro. "Support Vector Machine Applied to the Optimal Design of Composite Wing Panels." Aerospace 8, no. 11 (November 2, 2021): 328. http://dx.doi.org/10.3390/aerospace8110328.
Повний текст джерелаPigazzini, Marco S., Yuri Bazilevs, Andrew Ellison, and Hyonny Kim. "Isogeometric analysis for simulation of progressive damage in composite laminates." Journal of Composite Materials 52, no. 25 (April 22, 2018): 3471–89. http://dx.doi.org/10.1177/0021998318770723.
Повний текст джерелаRomano, Fulvio, Marco Barile, Gianpaolo Cacciapuoti, Jean-Luc Godard, Paolo Vollaro, and Philippe Barabinot. "Advanced OoA and Automated Technologies for the Manufacturing of a Composite Outer Wing Box." MATEC Web of Conferences 233 (2018): 00005. http://dx.doi.org/10.1051/matecconf/201823300005.
Повний текст джерелаJayasree, Nithin, Sadik Omairey, and Mihalis Kazilas. "Novel multi-zone self-heated composites tool for out-of-autoclave aerospace components manufacturing." Science and Engineering of Composite Materials 27, no. 1 (October 7, 2020): 325–34. http://dx.doi.org/10.1515/secm-2020-0033.
Повний текст джерелаRiccio, Aniello, Andrea Sellitto, Salvatore Saputo, Giovanni Conte, and Mauro Zarrelli. "Thermo-Mechanical Behaviour of a Composite Stiffened Panel Undergoing the Tail-Pipe Fire Event." Key Engineering Materials 774 (August 2018): 101–6. http://dx.doi.org/10.4028/www.scientific.net/kem.774.101.
Повний текст джерелаEsposito, Marco, Rinto Roy, Cecilia Surace, and Marco Gherlone. "Hybrid Shell-Beam Inverse Finite Element Method for the Shape Sensing of Stiffened Thin-Walled Structures: Formulation and Experimental Validation on a Composite Wing-Shaped Panel." Sensors 23, no. 13 (June 27, 2023): 5962. http://dx.doi.org/10.3390/s23135962.
Повний текст джерелаDaraji, Ali H., Jack M. Hale, and Jianqiao Ye. "Optimisation of energy harvesting for stiffened composite shells with application to the aircraft wing at structural flight frequency." Thin-Walled Structures 161 (April 2021): 107392. http://dx.doi.org/10.1016/j.tws.2020.107392.
Повний текст джерелаHiremath, Pavan, Sathyamangalam Ramanarayanan Viswamurthy, Manjunath Shettar, Nithesh Naik, and Suhas Kowshik. "Damage Tolerance of a Stiffened Composite Panel with an Access Cutout under Fatigue Loading and Validation Using FEM Analysis and Digital Image Correlation." Fibers 10, no. 12 (December 8, 2022): 105. http://dx.doi.org/10.3390/fib10120105.
Повний текст джерелаCestino, Enrico, Giacomo Frulla, Paolo Piana, and Renzo Duella. "Numerical/Experimental Validation of Thin-Walled Composite Box Beam Optimal Design." Aerospace 7, no. 8 (July 31, 2020): 111. http://dx.doi.org/10.3390/aerospace7080111.
Повний текст джерелаWang, Zhe, Xiangming Chen, Peng Zou, Xinxiang Li, Qingxianglong Liang, and Junchao Yang. "Parametric Analysis on Three-Points Bending Test of Typical Skin-Stringer Structure." Journal of Physics: Conference Series 2085, no. 1 (November 1, 2021): 012043. http://dx.doi.org/10.1088/1742-6596/2085/1/012043.
Повний текст джерелаFenner, Patrick, Andrew Watson, and Carol Featherston. "Modelling Infinite Length Panels Using the Finite Element Method." International Journal of Structural Stability and Dynamics 16, no. 07 (August 3, 2016): 1750038. http://dx.doi.org/10.1142/s0219455417500389.
Повний текст джерелаCapriotti, Margherita, and Francesco Lanza di Scalea. "Robust non-destructive inspection of composite aerospace structures by extraction of ultrasonic guided-wave transfer function in single-input dual-output scanning systems." Journal of Intelligent Material Systems and Structures 31, no. 5 (January 9, 2020): 651–64. http://dx.doi.org/10.1177/1045389x19898266.
Повний текст джерелаYu, Fei, Fei Yuan, Zhe Wang, and Xiangming Chen. "Experimental and Numerical Investigation on the Failure Behaviour of Multi-Stiffener Composite Panel Under Compression." Journal of Physics: Conference Series 2557, no. 1 (July 1, 2023): 012098. http://dx.doi.org/10.1088/1742-6596/2557/1/012098.
Повний текст джерелаLINDE, PETER. "VIRTUAL TESTING OF STIFFENED COMPOSITE PANELS AT AIRBUS." International Journal of Structural Stability and Dynamics 10, no. 04 (October 2010): 589–600. http://dx.doi.org/10.1142/s0219455410003634.
Повний текст джерелаPapadopoulos, F., D. Aiyappa, R. Shapriya, E. Sotirchos, H. Ghasemnejad, and R. Benhadj-Djilali. "Advanced Natural Stitched Composite Materials in Skin-Stiffener of Wind Turbine Blade Structures." Key Engineering Materials 525-526 (November 2012): 45–48. http://dx.doi.org/10.4028/www.scientific.net/kem.525-526.45.
Повний текст джерелаDoggui, Mohamed Montassar, Wael Touihri, Mondher Yahiaoui, and Moez Chafra. "Numerical investigation on aircraft wing stiffener composite material integration." Aerospace Systems 2, no. 2 (June 4, 2019): 137–45. http://dx.doi.org/10.1007/s42401-019-00027-9.
Повний текст джерелаPlenča, Stipe, and Albert Zamarin. "Structural Design of a Composite Trimaran." Journal of Maritime & Transportation Science 2, Special edition 2 (April 2018): 71–88. http://dx.doi.org/10.18048/2016-00.63.
Повний текст джерелаButler, R., M. Lillico, J. R. Banerjee, M. H. Patel, and G. T. S. Done. "Sequential use of conceptual MDO and panel sizing methods for aircraft wing design." Aeronautical Journal 103, no. 1026 (August 1999): 389–97. http://dx.doi.org/10.1017/s0001924000064617.
Повний текст джерелаDervilis, Nikolaos, R. Barthorpe, Wieslaw Jerzy Staszewski, and Keith Worden. "Structural Health Monitoring of Composite Material Typical of Wind Turbine Blades by Novelty Detection on Vibration Response." Key Engineering Materials 518 (July 2012): 319–27. http://dx.doi.org/10.4028/www.scientific.net/kem.518.319.
Повний текст джерелаKennedy, D., M. Fischer, and C. A. Featherston. "Recent developments in exact strip analysis and optimum design of aerospace structures." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 221, no. 4 (April 1, 2007): 399–413. http://dx.doi.org/10.1243/0954406jmes432.
Повний текст джерелаShahriari, Behrooz, Ali Nazari, and Mostafa Sahraei. "Buckling Analysis of A Composite Stiffend Panel Structure In The Aircraft’s Wing." Mechanic of Advanced and Smart Materials 2, no. 3 (November 22, 2022): 328–46. http://dx.doi.org/10.52547/masm.2.3.328.
Повний текст джерелаNavadeh, Navid, Ivan Goroshko, Yaroslav Zhuk, Farnoosh Etminan Moghadam, and Arash Soleiman Fallah. "Finite Element Analysis of Wind Turbine Blade Vibrations." Vibration 4, no. 2 (April 5, 2021): 310–22. http://dx.doi.org/10.3390/vibration4020020.
Повний текст джерелаTripathy, A. K., H. J. Patel, and S. S. Pang. "Bending Analysis of Laminated Composite Box Beams." Journal of Engineering Materials and Technology 116, no. 1 (January 1, 1994): 121–29. http://dx.doi.org/10.1115/1.2904247.
Повний текст джерелаZucco, G., V. Oliveri, M. Rouhi, R. Telford, G. Clancy, C. McHale, R. O’Higgins, T. M. Young, P. M. Weaver, and D. Peeters. "Static test of a variable stiffness thermoplastic composite wingbox under shear, bending and torsion." Aeronautical Journal 124, no. 1275 (January 22, 2020): 635–66. http://dx.doi.org/10.1017/aer.2019.161.
Повний текст джерелаSon, C. Y., H. I. Byun, K. H. Kim, J. K. Choi, and J. Y. Shin. "An Analysis and Experimental Study of the Rotor Blade with Composite Material Fiber Reinforced Plastics." Key Engineering Materials 306-308 (March 2006): 851–56. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.851.
Повний текст джерелаQiu, Zixue, Lei Qiu, Jiang Yuan, and Guan Lu. "On research of a phase synthesis time reversal focusing method for damage imaging of complex composite structures." Journal of Intelligent Material Systems and Structures 24, no. 2 (September 27, 2012): 209–25. http://dx.doi.org/10.1177/1045389x12461078.
Повний текст джерелаLee, Sang-Lae. "Active vibration suppression of wind turbine blades integrated with piezoelectric sensors." Science and Engineering of Composite Materials 28, no. 1 (January 1, 2021): 402–14. http://dx.doi.org/10.1515/secm-2021-0039.
Повний текст джерелаPark, Sunghyun, In-Gul Kim, Seokje Lee, and Oo-Chul Jun. "Optimal Design of the Composite Hat-shaped Stiffeners for Simplified Wing Box with Embedded Array Antenna." Journal of The Korean Society for Composite Materials 25, no. 6 (December 31, 2012): 224–29. http://dx.doi.org/10.7234/kscm.2012.25.6.224.
Повний текст джерелаQiu, Lei, Shen Fang Yuan, and Tian Xiang Huang. "A Time Reversal Imaging Method without Relying on Transfer Function for Impact and Damage Monitoring of Composite Structures." Applied Mechanics and Materials 330 (June 2013): 542–48. http://dx.doi.org/10.4028/www.scientific.net/amm.330.542.
Повний текст джерелаMandell, John F., Douglas S. Cairns, Daniel D. Samborsky, Robert B. Morehead, and Darrin J. Haugen. "Prediction of Delamination in Wind Turbine Blade Structural Details." Journal of Solar Energy Engineering 125, no. 4 (November 1, 2003): 522–30. http://dx.doi.org/10.1115/1.1624613.
Повний текст джерелаLiu, Dianzi, Chuanwei Zhang, Z. Wan, and Z. Du. "Topology optimization of a novel fuselage structure in the conceptual design phase." Aircraft Engineering and Aerospace Technology 90, no. 9 (November 14, 2018): 1385–93. http://dx.doi.org/10.1108/aeat-04-2017-0100.
Повний текст джерелаStanford, Bret K., and Christine V. Jutte. "Comparison of curvilinear stiffeners and tow steered composites for aeroelastic tailoring of aircraft wings." Computers & Structures 183 (April 2017): 48–60. http://dx.doi.org/10.1016/j.compstruc.2017.01.010.
Повний текст джерелаBarkanov, E., E. Eglītis, F. Almeida, M. C. Bowering, and G. Watson. "Optimal design of composite upper covers of lateral wings with the effect of rib attachment to stiffener webs." Mechanics of Composite Materials 49, no. 3 (July 2013): 285–96. http://dx.doi.org/10.1007/s11029-013-9345-3.
Повний текст джерелаSilva, Fernando José, Bernardo Félix Santiago Lana, Francisco Carlos Rodrigues, and Luís Eustáquio Moreira. "Buckling of Bamboo Masts with Interposed Spacers." Key Engineering Materials 634 (December 2014): 389–99. http://dx.doi.org/10.4028/www.scientific.net/kem.634.389.
Повний текст джерелаPetrolo, Marco, and Erasmo Carrera. "High-Fidelity and Computationally Efficient Component-Wise Structural Models: An Overview of Applications and Perspectives." Applied Mechanics and Materials 828 (March 2016): 175–96. http://dx.doi.org/10.4028/www.scientific.net/amm.828.175.
Повний текст джерелаQian, Xiuyang, Yushan Zhou, Menghui Wang, Liya Cai, and Feng Pei. "Structural design of composite stiffened panel for a flat wing micro-aircraft." SN Applied Sciences 2, no. 4 (March 20, 2020). http://dx.doi.org/10.1007/s42452-020-2559-9.
Повний текст джерела