Добірка наукової літератури з теми "Stiffened composite panel"
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Статті в журналах з теми "Stiffened composite panel"
Shao, Qing, Yu Ting He, Teng Zhang, Hai Wei Zhang, and Qing Shan Kang. "Simulation of Compress Buckling Performance of Composite Stiffened Panel." Applied Mechanics and Materials 184-185 (June 2012): 1189–93. http://dx.doi.org/10.4028/www.scientific.net/amm.184-185.1189.
Повний текст джерелаMoorhouse, Anna, Micah Shepherd, and Benjamin S. Beck. "Incorporation of acoustic black hole stiffeners into composite airframes for reduction of noise radiation." Journal of the Acoustical Society of America 151, no. 4 (April 2022): A129—A130. http://dx.doi.org/10.1121/10.0010875.
Повний текст джерелаZhao, Chuang, Zhi Dong Guan, and Xia Guo. "Compression Performance of Repaired Composite Stiffened Panels: Bolted Repair and Scarfed Bonded Repair." Materials Science Forum 813 (March 2015): 152–60. http://dx.doi.org/10.4028/www.scientific.net/msf.813.152.
Повний текст джерелаLiu, Jun, Bao Zong Huang, and Ge Lan Li. "Secondary Buckling and Progressive Failure Analysis of Tailored Composite Panels in Thin-Walled Box-Shape Composite Beams under Bending and Torsion." Advanced Materials Research 41-42 (April 2008): 445–48. http://dx.doi.org/10.4028/www.scientific.net/amr.41-42.445.
Повний текст джерелаCherniaev, Aleksandr. "A new laminates encoding scheme for the genetic algorithm-based optimization of stiffened composite panels." Engineering Computations 31, no. 1 (February 25, 2014): 33–47. http://dx.doi.org/10.1108/ec-08-2011-0089.
Повний текст джерелаSanchez-Carmona, Alejandro, and Cristina Cuerno-Rejado. "Composite stiffened panel sizing for conceptual tail design." Aircraft Engineering and Aerospace Technology 90, no. 8 (November 5, 2018): 1272–81. http://dx.doi.org/10.1108/aeat-05-2017-0129.
Повний текст джерелаSahadevan, 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 джерелаLi, Yeou-Fong, Habib Meda, and Walter Chen. "The Design and Analysis of Internally Stiffened GFRP Tubular Decks—A Sustainable Solution." Sustainability 10, no. 12 (December 1, 2018): 4538. http://dx.doi.org/10.3390/su10124538.
Повний текст джерелаGuofan, Zhang, Wan Chunhua, and Nie Xiaohua. "Study on compressive bearing capacity and efficiency of composite stiffened panels with different cross-sections." Journal of Physics: Conference Series 2336, no. 1 (August 1, 2022): 012027. http://dx.doi.org/10.1088/1742-6596/2336/1/012027.
Повний текст джерелаKALNINS, KASPARS, ROLANDS RIKARDS, JANIS AUZINS, CHIARA BISAGNI, HAIM ABRAMOVICH, and RICHARD DEGENHARDT. "METAMODELING METHODOLOGY FOR POSTBUCKLING SIMULATION OF DAMAGED COMPOSITE STIFFENED STRUCTURES WITH PHYSICAL VALIDATION." International Journal of Structural Stability and Dynamics 10, no. 04 (October 2010): 705–16. http://dx.doi.org/10.1142/s0219455410003695.
Повний текст джерелаДисертації з теми "Stiffened composite panel"
Liu, Yifei. "Optimum design of a composite outer wing subject to stiffness and strength constraints." Thesis, Cranfield University, 2011. http://dspace.lib.cranfield.ac.uk/handle/1826/6833.
Повний текст джерелаZhao, Wei. "Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings." Diss., Virginia Tech, 2017. http://hdl.handle.net/10919/79143.
Повний текст джерелаPh. D.
Jrad, Mohamed. "Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures." Diss., Virginia Tech, 2015. http://hdl.handle.net/10919/52276.
Повний текст джерелаPh. D.
Shenoy, Sudhir Lankarani Hamid M. "Energy absorption of a car roof reinforced with a grid stiffened composite panel in the event of a rollover." Diss., Click here for available full-text of this thesis, 2006. http://library.wichita.edu/digitallibrary/etd/2006/t073.pdf.
Повний текст джерела"May 2006." Title from PDF title page (viewed on October 29, 2006). Thesis adviser: Hamid M. Lankarani. Includes bibliographic references (leaves 57-59).
Shenoy, Sudhir Shivaraya. "Energy absorption of a car roof reinforced with a grid stiffened composite panel in the event of a rollover." Thesis, Wichita State University, 2006. http://hdl.handle.net/10057/386.
Повний текст джерелаThesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering
"May 2006."
Includes bibliographic references (leaves 57-59)
Cil, Kursad. "Free Flexural (or Bending) Vibrations Analysis Of Doubly Stiffened, Composite, Orthotropic And/or Isotropic Base Plates And Panels (in Aero-structural Systems)." Master's thesis, METU, 2003. http://etd.lib.metu.edu.tr/upload/2/1062256/index.pdf.
Повний текст джерелаs Solutions can be applied in that direction. Thus, the transverse shear deformations and the rotary moments of inertia of plates are included in the formulation. The very thin, yet elastic deformable adhesive layers are considered as continua with transverse normal and shear stresses. The damping effects in the plates and the adhesive layers are neglected. The sets of the systems of equations of the Mindlin Plate Theory are reduced to a set of the Governing System of First Order Ordinary Differential Equations in the state vector form. The sets of the Governing System for each Main PROBLEM constitute a Two-Point Boundary Value Problem in the y-direction which is taken along the length of the plates. Then, the system is solved by the Modified Transfer Matrix Method (with Interpolation Polynomials and/or Chebyshev Polynomials)which is a relatively semi-analytical and numerical technique. The numerical results and important parametric studies of the natural modes and the corresponding frequencies of the composite system are presented.
Cohen, David. "Calculation of skin-stiffener interface stresses in stiffened composite panels." Diss., Virginia Polytechnic Institute and State University, 1987. http://hdl.handle.net/10919/82897.
Повний текст джерелаPh. D.
Grall, Bruno. "Structural analysis of geodesically stiffened composite panels with variable stiffener distribution." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-12232009-020522/.
Повний текст джерелаUzman, Burak Jr. "Thermal Analysis and Response of Grid-Stiffened Composite Panels." Thesis, Virginia Tech, 1997. http://hdl.handle.net/10919/31381.
Повний текст джерелаMaster of Science
Henderson, Joseph Lynn. "Combined structural and manufacturing optimization of stiffened composite panels." Thesis, This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-09182008-063429/.
Повний текст джерелаКниги з теми "Stiffened composite panel"
L, Phillips John. Structural analysis and optimum design of geodesically stiffened composite panels. Blacksburg, Va: Virginia Polytechnic Institute and State University, Center for Composite Materials and Structures, 1990.
Знайти повний текст джерелаSimitses, George J. Buckling of delaminated long panels under pressure and of radially-loaded stiffened annular plates. Atlanta, Ga: Georgia Institute of Technology, 1985.
Знайти повний текст джерелаLevon, Minnetyan, and United States. National Aeronautics and Space Administration., eds. Discontinuously stiffened composite panel under compressive loading. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаDetailed analysis and test correlation of a stiffened composite wing panel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration., eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаW, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаCalculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаCalculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.
Знайти повний текст джерелаStructural analysis and design of geodesically stiffened composte panels with variable stiffener distribution. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаЧастини книг з теми "Stiffened composite panel"
Wiggenraad, J. F. M., and N. R. Bauld. "Interlaminar Stress Analysis at the Skin/Stiffener Interface of a Grid-Stiffened Composite Panel." In Composite Structures, 415–31. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_32.
Повний текст джерелаTserpes, Konstantinos, Elli Moutsompegka, Mareike Schlag, Kai Brune, Christian Tornow, Ana Reguero Simón, and Romain Ecault. "Characterization of Pre-bond Contamination and Aging Effects for CFRP Bonded Joints Using Reference Laboratory Methods, Mechanical Tests, and Numerical Simulation." In Adhesive Bonding of Aircraft Composite Structures, 51–117. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_2.
Повний текст джерелаIndira, Sai, D. Mallikarjuna Reddy, Jayakrishna Kandasamy, M. Rajesh, Vishesh Ranjan Kar, and M. T. H. Sultan. "Damage Characterization of Composite Stiffened Panel Subjected to Low Velocity Impact." In Structural Health Monitoring System for Synthetic, Hybrid and Natural Fiber Composites, 37–50. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-8840-2_4.
Повний текст джерелаPark, Chan Yik. "Damage Index Comparison for a Composite Stiffened Panel Using Lamb Wave." In Advanced Materials Research, 1265–68. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-463-4.1265.
Повний текст джерелаBi, Xue, Peng Zou, and Xiangming Chen. "Study on Bearing Mechanism of Composite Stiffened Panel with Delamination Under Shear Load." In Mechanical Engineering and Materials, 155–72. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-68303-0_13.
Повний текст джерелаEl Samrout, Ahmad, Oussama Braydi, Rafic Younes, Francois Trouchu, and Pascal Lafon. "A New Hybrid Method to Solve the Multi-objective Optimization Problem for a Composite Hat-Stiffened Panel." In Bioinspired Heuristics for Optimization, 77–88. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-95104-1_5.
Повний текст джерелаSmith, C. S., and R. S. Dow. "Interactive Buckling Effects in Stiffened FRP Panels." In Composite Structures 4, 122–37. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3455-9_9.
Повний текст джерелаSmith, C. S., and R. S. Dow. "Compressive Strength of Longitudinally Stiffened GRP Panels." In Composite Structures 3, 468–90. Dordrecht: Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2_33.
Повний текст джерелаTripathy, Biswajit, and K. P. Rao. "Optimum Design for Buckling of Plain and Stiffened Composite Cylindrical Panels." In Composite Structures, 371–81. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_29.
Повний текст джерелаChandra, K. S. Subash, T. Rajanna, and K. Venkata Rao. "Thermal Buckling Analysis of Stiffened Composite Cutout Panels." In Recent Trends in Construction Technology and Management, 935–48. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2145-2_69.
Повний текст джерелаТези доповідей конференцій з теми "Stiffened composite panel"
Kidane, Samuel, Eyassu Woldesenbet, Guoqiang Li, Jack Helms, and Brett H. Smith. "Preliminary Analysis of Grid Stiffened Composite Cylinders." In ASME 2002 Engineering Technology Conference on Energy. ASMEDC, 2002. http://dx.doi.org/10.1115/etce2002/ot-29153.
Повний текст джерелаYuceoglu, Umur, Jaber Javanshir, and O¨zen Guvendik. "On a General Approach to Free Vibrations Response of Integrally-Stiffened and/or Stepped-Thickness Rectangular Plates or Panels." In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-66980.
Повний текст джерелаBROER, AGNES, NAN YUE, GEORGIOS GALANOPOULOS, RINZE BENEDICTUS, THEODOROS LOUTAS, and DIMITRIOS ZAROUCHAS. "ON THE CHALLENGES OF UPSCALING DAMAGE MONITORING METHODOLOGIES FOR STIFFENED COMPOSITE AIRCRAFT PANELS." In Structural Health Monitoring 2021. Destech Publications, Inc., 2022. http://dx.doi.org/10.12783/shm2021/36237.
Повний текст джерелаSundararaj, K., and M. Ganesh. "Numerical investigation of composite stiffened panel with various stiffeners under axial compression." In PROCEEDINGS OF ADVANCED MATERIAL, ENGINEERING & TECHNOLOGY. AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0019625.
Повний текст джерелаAkula, Venkata M. K. "Low-Velocity Impact Analysis of a Stiffened Composite Panel." In ASME 2015 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/pvp2015-45727.
Повний текст джерелаMucha, Waldemar, Wacław Kuś, Júlio C. Viana, and João Pedro Nunes. "Comparison of numerical and experimental strain distributions in composite panel for aerospace applications." In VI ECCOMAS Young Investigators Conference. València: Editorial Universitat Politècnica de València, 2021. http://dx.doi.org/10.4995/yic2021.2021.12572.
Повний текст джерелаUmezawa, Keisuke, and Takahira Aoki. "Postbuckling Analysis of Composite Stiffened Panel under Shear Load." In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1432.
Повний текст джерелаTaki, Toshimi, and Tomohiro Kitagawa. "Postbuckling strength of composite stiffened panel under shear load." In Aircraft Engineering, Technology, and Operations Congress. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-3934.
Повний текст джерелаAbramovich, Haim, Chiara Bisagni, and Potito Cordisco. "Post-Buckling Test Simulation of a Stiffened Composite Panel." In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-2126.
Повний текст джерелаRout, Mrutyunjay, Sasank Shekhar Hota, and Amit Karmakar. "Multiple Low Velocity Impact on Twisted Composite Stiffened Blade: A Finite Element Approach." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4772.
Повний текст джерела