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Journal articles on the topic 'Composite wing rib post'

Author: Grafiati

Published: 4 June 2021

Last updated: 17 February 2022

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1

Hu, Zheng, and Olexii Vambol. "TOPOLOGICAL DESIGNING AND ANALYSIS OF THE COMPOSITE WING RIB." Aerospace technic and technology, no. 6 (November 27, 2020): 4–14. http://dx.doi.org/10.32620/aktt.2020.6.01.

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The composite structures in the aerospace industry for in recent decades are widely applied however, at the beginning of the 21st century composites are growing rapidly. The largest companies in the aerospace industry are increasing the volume of composites application of in the structures, and nowadays the volume of composites reaches 50%. The different elements of aircraft and even highly loaded structures such as spars, ribs, skin, etc., are currently made from composites. First of all, this is due to the possibility of a significant reduction in the weight of the structure, as well as a de

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2

Yang, Kang, Yi-lin Guo, Dong-hui Li, et al. "Design and static testing of wing structure of a composite four-seater electric aircraft." Science and Engineering of Composite Materials 27, no. 1 (2020): 258–63. http://dx.doi.org/10.1515/secm-2020-0023.

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AbstractBecause of its light weight, high strength, designable, composite materials are more and more widely used in the field of aerospace, especially in the field of general aviation. In this paper, the structural design and analysis of the composite wing (include wing beam, rib, skin, leading edge and trailing edge) of a four-seater electric aircraft were carried out. The finite element numerical analysis model of the composite wing was established, and the deformation and strain distribution of the composite wing under the limited load required by airworthiness regulations were calculated.

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Yang, Kang, Liguo Zhang, Shude Ji, Yumei Yue, and Wang Ji. "Static Testing and Analysis of Composite Wing of a Two-Seater Aircraft Powered by Li-Ion Battery Electric Propulsion." Advanced Composites Letters 25, no. 6 (2016): 096369351602500. http://dx.doi.org/10.1177/096369351602500601.

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The present paper studied the strength and deformation characteristics of a composite wing of a two-seater aircraft powered by Li-ion battery electric propulsion. In order to get the airworthiness certificate, the static testing is indispensable. The primary wing structure component includes upper and lower skins, leading edge, trailing edge, a root rib and main spar. The main purpose of static testing is to examine the bending strength of the wing. The testing results are in good agreement with the FE analysis results and the bending strength of wing is strong enough to support the limit load

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Гребеников, А. Г., Ю. В. Дьяченко, В. В. Коллеров, И. В. Малков, Н. И. Москаленко та В. А. Урбанович. "КОНСТРУКТИВНО-ТЕХНОЛОГІЧНІ ОСОБЛИВОСТІ НЕСУЧИХ ПОВЕРХОНЬ ВЕРТОЛЬОТА З ПОЛІМЕРНИХ КОМПОЗИЦІЙНИХ МА-ТЕРІАЛІВ". Open Information and Computer Integrated Technologies, № 84 (2 липня 2019): 4–49. http://dx.doi.org/10.32620/oikit.2019.84.01.

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The analysis of both foreign and domestic experience in the use of polymer composite materials in the structures of the lifting surfaces of a helicopter (blades, wing, stabilizer, fin), as well as the technological features of the manufacture of such structures is performed. The design and technological and operational advantages and disadvantages of composite blades compared to all-metal blades are noted. The load-carrying structures of the composite main rotor blades of a helicopter, as well as the schemes of special joints of the MR blade and the polymer composite materials package are cons

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Krupa, Eduardo P., Jonathan E. Cooper, Alberto Pirrera, and Raj Nangia. "Improved aerostructural performance via aeroservoelastic tailoring of a composite wing." Aeronautical Journal 122, no. 1255 (2018): 1442–74. http://dx.doi.org/10.1017/aer.2018.66.

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ABSTRACTThis paper investigates the synergies and trade-offs between passive aeroelastic tailoring and adaptive aeroelastic deformation of a transport composite wing for fuel burn minimisation. This goal is achieved by optimising thickness and stiffness distributions of constitutive laminates, jig-twist shape and distributed control surface deflections through different segments of a nominal “cruise-climb” mission. Enhanced aerostructural efficiency is sought both passively and adaptively as a means of aerodynamic load redistribution, which, in turn, is used for manoeuvre load relief and minim

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Gantois, K., and A. J. Morris. "Incorporation of manufacturing information into an MDO environment." Aeronautical Journal 103, no. 1026 (1999): 383–88. http://dx.doi.org/10.1017/s0001924000064605.

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Abstract The Paper describes a metal and composite recurrent cost model of a large civil aircraft wing structure for a multidisciplinary design, analysis and optimisation (MDO) environment. The work was part of a recent European MDO project (BE95-2056) which investigated methods for the integration of structures, aerodynamics, dynamics and manufacturing cost at the preliminary design stage. The paper discusses the cost modelling approach, which is based on parametric and process cost model methods, and the integration of the cost models into an MDO process. Results for the cost models are show

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Goonewardene, L. A., M. A. Price, M. F. Liu, R. T. Berg, and C. M. Erichsen. "A study of growth and carcass traits in dehorned and polled composite bulls." Canadian Journal of Animal Science 79, no. 3 (1999): 383–85. http://dx.doi.org/10.4141/a98-121.

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Phenotypically dehorned (genetically horned) and polled bulls were similar for birth, weaning weight, pre- and post-weaning ADG, carcass weight, grade fat, marbling, rib-eye area, cutability and carcass grade. Polled bulls had higher (P < 0.02) fat over the rib-eye compared with dehorned. The similarity in growth and a majority of carcass traits between polled and horned, would suggest that breeding for polledness may be recommended to eliminate horns. Key words: Dehorned, polled, growth, carcass traits, bulls

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8

Sivakumar, V., Khooshboo P. Dani, and Suddapally Sriram. "Prediction of Stress Intensity Factor on Precracked Composite Wing Rib Made up of Carbon-Epoxy IM7-8552." Journal of Failure Analysis and Prevention 16, no. 4 (2016): 635–46. http://dx.doi.org/10.1007/s11668-016-0130-1.

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9

Breen, John E., Michael E. Kreger, Christopher D. White, and Gordon C. Clark. "Field evaluation and model test of a composite wing-girder bridge." Canadian Journal of Civil Engineering 14, no. 6 (1987): 753–62. http://dx.doi.org/10.1139/l87-113.

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This paper presents the key observations and conclusions from the evaluation of an innovative "loose-fit" composite, post-tensioned concrete wing-girder bridge proposed for an elevated interstate highway expansion in an urban environment. The evaluation program included both testing to destruction of a 1/2-scale model of a partial span as well as construction monitoring and field testing at service load levels of a full-scale prototype two-span bridge. Results of both construction measurements and loading tests were compared with analytical predictions. Laboratory tests showed the composite be

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10

Latif, R. F., M. K. A. Khan, A. Javed, S. I. A. Shah, and S. T. I. Rizvi. "A semi-analytical approach for flutter analysis of a high-aspect-ratio wing." Aeronautical Journal 125, no. 1284 (2020): 410–29. http://dx.doi.org/10.1017/aer.2020.71.

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AbstractWe present a hybrid, semi-analytical approach to perform an eigenvalue-based flutter analysis of an Unmanned Aerial Vehicle (UAV) wing. The wing has a modern design that integrates metal and composite structures. The stiffness and natural frequency of the wing are calculated using a Finite Element (FE) model. The modal parameters are extracted by applying a recursive technique to the Lanczos method in the FE model. Subsequently, the modal parameters are used to evaluate the flutter boundaries in an analytical model based on the p-method. Two-degree-of-freedom bending and torsional flut

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Mitrofanov, O., and O. Mazen. "Designing of Thin Composite Panels with the Post-Buckling Behavior Considering Rigid Support and Loading with Shear Flows." Key Engineering Materials 887 (May 2021): 657–61. http://dx.doi.org/10.4028/www.scientific.net/kem.887.657.

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Geometrically non-linear problem of orthotropic thin rectangular panel post-buckling behavior with shear is solved. Deflection function takes all-boundary rigid support conditions into account. Based on derived solution method of smooth panels design which can be used for aircraft structures rib and spar webs optimal parameters is suggested.

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12

Wang, Peiyan, Xinting Huang, Zhongnan Wang, Xiaoliang Geng, and Yuansheng Wang. "Buckling and Post-Buckling Behaviors of a Variable Stiffness Composite Laminated Wing Box Structure." Applied Composite Materials 25, no. 2 (2017): 449–67. http://dx.doi.org/10.1007/s10443-017-9643-3.

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Xia, Shao Quan, Jian Chun Xiao, and Ke Jian Ma. "Formation and Specialties of Steel / RC Composite Open-Web Floor Structures." Advanced Materials Research 476-478 (February 2012): 1572–76. http://dx.doi.org/10.4028/www.scientific.net/amr.476-478.1572.

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A new type of steel / reinforced concrete composite open-web floor / roof structure is proposed. Its formation is a two-way intersectant open-web beam plate. The lower layer is a rib lattice that is composed of U-style steel slabs infilled with RC, the upper layer is assembled with pre-cast RC slabs and post-cast RC ribs, the connections of upper layer and lower layer are RC shear-bearing blocks. The plate has the specialties of lightweight, simple inside sight sense, high stiffness-weight ratio, and less seismic inertial force. Its formation, construction process, design method and main mecha

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Lee, Yoonho, Jihyuk Kim, and Euitae Lee. "Lengthening of the Postoperative Short Nose: Combined Use of a Gull-Wing Concha Composite Graft and a Rib Costochondral Dorsal Onlay Graft." Plastic & Reconstructive Surgery 105, no. 6 (2000): 2190–99. http://dx.doi.org/10.1097/00006534-200005000-00045.

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15

Kumar, S. Anoop, R. Rajesh, and S. Pugazhendhi. "A review of stress concentration studies on fibre composite panels with holes/cutouts." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 234, no. 11 (2020): 1461–72. http://dx.doi.org/10.1177/1464420720944571.

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Composite panels are widely used as structural members due to their high strength-to-weight ratio. In order to reduce further weight, cutouts or notches are introduced in these members. These cutouts also serve utility requirements such as man-holes for purpose of service as well as for passing electric or fuel lines. An aircraft wing rib is a typical example of such a composite panel. Even while composites with holes or cutouts provide great savings in weight compared to metallic structures, the presence of holes itself leads to strength reduction. The reduction in strength is due to the conc

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Pigazzini, 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 (2018): 3471–89. http://dx.doi.org/10.1177/0021998318770723.

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The increasing popularity of composite materials in aerospace applications is creating the need for a new class of predictive methods and tools for the simulation of progressive damage in laminated fiber-reinforced composite structures. The unique challenges associated with modeling damage in these structures may be addressed by means of thin-shell formulations which are naturally developed in the context of Isogeometric Analysis. In this paper, we further validate our recently developed Isogeometric Analysis-based multi-layer shell model for progressive damage simulations using experimental d

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17

Na, Y. H., J. H. Kim, and S. J. Shin. "Vibration analyses of an equivalent plate wing with an external store." Aeronautical Journal 118, no. 1207 (2014): 1090–98. http://dx.doi.org/10.1017/s0001924000009763.

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Generally, pylon-mounted external stores significantly affect the aerodynamic characteristics of the aircraft due to their flexibility. Therefore, many investigations upon the dynamic and aeroelastic characteristics of an aircraft wing with external stores have been done over the last few decades Recently, a study was carried out regarding the aeroelastic effects on wings by the engine placement For severe operation conditions, classical linear theory with a small amount of amplitude vibration may not be an appropriate analysis. Nonlinear vibration analysis will be required, especially when th

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18

Marzani, Alessandro, Nicola Testoni, Luca De Marchi, Marco Messina, Ernesto Monaco, and Alfonso Apicella. "An open database for benchmarking guided waves structural health monitoring algorithms on a composite full-scale outer wing demonstrator." Structural Health Monitoring 19, no. 5 (2019): 1524–41. http://dx.doi.org/10.1177/1475921719889029.

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This article reports on the creation of an open database of piezo-actuated and piezo-received guided wave signals propagating in a composite panel of a full-scale aeronautical structure. The composite panel closes the bottom part of a wingbox that, along with the leading edge, the trailing edge, and the wingtip, forms an outer wing demonstrator approximately 4.5 m long and from 1.2 to 2.3 m wide. To create the database, a structural health monitoring system, composed of a software/hardware central unit capable of controlling a network of 160 piezoelectric transducers secondarily bonded on the

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19

Esola, Shane, Brian Wisner, Prashanth Vanniamparambil, John Geriguis, and Antonios Kontsos. "Part Qualification Methodology for Composite Aircraft Components Using Acoustic Emission Monitoring." Applied Sciences 8, no. 9 (2018): 1490. http://dx.doi.org/10.3390/app8091490.

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The research presented in this article aims to demonstrate how acoustic emission (AE) monitoring can be implemented in an industrial setting to assist with part qualification, as mandated by related industry standards. The combined structural and nondestructive evaluation method presented departs from the traditional pass/fail criteria used for part qualification, and contributes toward a multi-dimensional assessment by taking advantage of AE data recorded during structural testing. To demonstrate the application of this method, 16 composite fixed-wing-aircraft spars were tested using a struct

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20

Chang, Yu Zhen, and Ling Ling Wang. "The Influence of Different Restrained Boundary Conditions on the Stability of Steel-Concrete Composite Ribbed Shell." Advanced Materials Research 243-249 (May 2011): 7005–8. http://dx.doi.org/10.4028/www.scientific.net/amr.243-249.7005.

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The steel-concrete composite ribbed shell is a new type of spatial structure. Different restrained boundary conditions have a considerably influence on the ultimate bearing capacity and stability. Based on the nonlinear finite element method, a numerical model is made by finite element analysis software ANSYS, in which material and geometrical nonlinear are considered. A spherical composite ribbed shell with 40m span, three different section dimensions and two different vector heights is used as an example, in which 4 different restrained boundary conditions are considered, including all fixed

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21

Cervantes, Miguel A., Michelle R. Garcia, Brittney N. Keel, William T. Oliver, James E. Wells, and Lea A. Rempel. "PSI-16 Sow parity structure and body condition measurements throughout lactation and relationship to piglet growth." Journal of Animal Science 97, Supplement_2 (2019): 250–51. http://dx.doi.org/10.1093/jas/skz122.441.

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Abstract Energy demands during lactation can greatly influence sow body condition and piglet performance. Therfore, it was hypothesized that primiparous sows would have reduced sow body condition measurements and piglet growth. Eight weekly farrowing seasons (N=157 dams) were used to evaluate sow body condition (Post Farrowing; PF to Weaning; WN) and piglet growth. Final number of white composite sows within parity were as follows: Parity 1(P1), 62; P2, 50; P3, 30; and P4, 15. Body condition was measured at PF and WN using sow calipers (last rib and hip) and 10th rib ultrasound. Sows were cate

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22

de Corte, Wouter, Arne Jansseune, Veerle Boel, and Giovanni Martinola. "Properties of Fiber Reinforced High Performance Cement Based Overlays for Orthotropic Bridge Decks." Key Engineering Materials 713 (September 2016): 236–39. http://dx.doi.org/10.4028/www.scientific.net/kem.713.236.

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An increasing number of steel orthotropic bridge deck require repair due to fatigue cracking. For the rib to deckplate joint, a possible solution is to reinforce the fatigue prone deck plate by replacing the asphalt wearing surface with a reinforced high strength concrete overlay. However, this process has been proven very difficult to execute and consequently has some issues regarding durability. This paper reports on high performance fiber reinforced cement based overlay solutions with gritted epoxy interlayer for a typical orthotropic deck with inadequate plate dimensions. Material characte

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23

Tabbal, Nicolas. "Lengthening of the Postoperative Short Nose: Combined Use of a Gull-Wing Concha Composite Graft and a Rib Costochondral Dorsal Onlay Graft by Yoonho Lee, M.D., Ph.D., Jihyuk Kim, M.D., and Euitae Lee, M.D." Plastic & Reconstructive Surgery 105, no. 6 (2000): 2200–2201. http://dx.doi.org/10.1097/00006534-200005000-00046.

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24

Paternoster, Henry John, Deborah Warr, and Keith Jacobs. "The enigma of the bogan and its significance to class in Australia: A socio-historical analysis." Journal of Sociology 54, no. 3 (2018): 429–45. http://dx.doi.org/10.1177/1440783318769752.

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This analysis offers a historical perspective to chart the contested discourses that inform understandings of the figure of the ‘bogan’, suggesting its evocation reflects unresolved tensions and accumulated meanings left by the various reconfigurations of class politics since colonial settlement in Australia. We focus on three key historical periods to show how socio-political formations influence both classed identities and class relations: the 1890s, when the ethos of the labour movement was established as the central imaginative motif of a nascent Australian nation; the post-war years, when

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25

Fenner, 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 (2016): 1750038. http://dx.doi.org/10.1142/s0219455417500389.

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This paper compares three finite element models for determining the buckling and post-buckling performance of infinite length thin walled composite and metal stiffened panels — such as for modeling theoretical aircraft upper wing skin panels — namely single bay, double half-bay and quad half-bay models. The quad half-bay model is shown to be the ideal model as all wavelengths of buckling are permitted. This model gives an accurate estimate of postbuckling behavior that can include advanced behavior such as mode jumping or collapse while the single bay and double half-bay models are more restri

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26

Fursov, A. Yu. "The operation of the cone shell blocks of offshore structures under ice impact." Oil and Gas Studies, no. 3 (July 8, 2020): 63–74. http://dx.doi.org/10.31660/0445-0108-2020-3-63-74.

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The prospects for the development of the Azov-Black sea region of the Russian Federation are primarily related to the development of the deep-water part of the Black Sea. In general, the forecast hydrocarbon resources are estimated at 1,5-2,4 trillion m3 in gas equivalent. Ice loads are one of the most important factors determining the stress state of the entire stationary platform when developing and designing offshore structures for the gas field in the Sea of Azov. The author of the article proposes to install special structures, such as cone icebreaking devices, at the contact points. An a

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27

Barwick, S. A., M. L. Wolcott, D. J. Johnston, H. M. Burrow, and M. T. Sullivan. "Genetics of steer daily and residual feed intake in two tropical beef genotypes, and relationships among intake, body composition, growth and other post-weaning measures." Animal Production Science 49, no. 6 (2009): 351. http://dx.doi.org/10.1071/ea08249.

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Genetic parameters for Brahman (BRAH) and Tropical Composite (TCOMP) cattle were estimated for steer production traits recorded at weaning (WEAN), 80 days post-weaning (POSTW), feedlot entry (ENTRY) and after ∼120 days feedlot finishing (EXIT). The TCOMP was 50% Bos indicus, African Sanga or other tropically adapted Bos taurus, and 50% non-tropically adapted Bos taurus. Data involved 2216 steers, comprising 1007 BRAH by 53 sires and 1209 TCOMP by 50 sires. Individual daily feed intake (DFI) and residual feed intake (RFI) were assessed on 680 BRAH and 783 TCOMP steers over an ~70-day feedlot te

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28

Raeside, M. C., M. Robertson, Z. N. Nie, D. L. Partington, J. L. Jacobs, and R. Behrendt. "Dietary choice and grazing behaviour of sheep on spatially arranged pasture systems. 2. Wether lamb growth and carcass weight at slaughter." Animal Production Science 57, no. 4 (2017): 710. http://dx.doi.org/10.1071/an15540.

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Dry matter production and nutritive characteristics of the pasture feedbase during autumn are key drivers of profitability in Australia’s prime lamb systems. An experiment was conducted to test the hypothesis that offering lambs dietary choice through spatially separated combinations of perennial ryegrass (Lolium perenne L.), plantain (Plantago lanceolata L.) and/or lucerne (Medicago sativa L.) improves the post-weaning liveweight gain, condition score (CS), pre- and post-slaughter carcass characteristics and reduces the internal parasite burdens of wether lambs finished to a slaughter weight

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Barwick, S. A., D. J. Johnston, H. M. Burrow, et al. "Genetics of heifer performance in 'wet' and 'dry' seasons and their relationships with steer performance in two tropical beef genotypes." Animal Production Science 49, no. 6 (2009): 367. http://dx.doi.org/10.1071/ea08273.

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The genetics of heifer performance in tropical ‘wet’ and ‘dry’ seasons, and relationships with steer performance, were studied in Brahman (BRAH) and Tropical Composite (TCOMP) (50% Bos indicus, African Sanga or other tropically adapted Bos taurus; 50% non-tropically adapted Bos taurus) cattle of northern Australia. Data were from 2159 heifers (1027 BRAH, 1132 TCOMP), representing 54 BRAH and 51 TCOMP sires. Heifers were assessed after post-weaning ‘wet’ (ENDWET) and ‘dry’ (ENDDRY) seasons. Steers were assessed post-weaning, at feedlot entry, over a 70-day feed test, and after ∼120-day finishin

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Barwick, S. A., D. J. Johnston, H. M. Burrow, et al. "Erratum to: Genetics of heifer performance in 'wet' and 'dry' seasons and their relationships with steer performance in two tropical beef genotypes." Animal Production Science 49, no. 8 (2009): 727. http://dx.doi.org/10.1071/ea08273_er.

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The genetics of heifer performance in tropical 'wet' and 'dry' seasons, and relationships with steer performance, were studied in Brahman (BRAH) and Tropical Composite (TCOMP) (50% Bos indicus, African Sanga or other tropically adapted Bos taurus; 50% non-tropically adapted Bos taurus) cattle of northern Australia. Data were from 2159 heifers (1027 BRAH, 1132 TCOMP), representing 54 BRAH and 51 TCOMP sires. Heifers were assessed after post-weaning 'wet' (ENDWET) and 'dry' (ENDDRY) seasons. Steers were assessed post-weaning, at feedlot entry, over a 70-day feed test, and after ~120-day finishin

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31

Miletic, Sasa. "Acting Out: "Cage Rage" and the Morning After." M/C Journal 22, no. 1 (2019). http://dx.doi.org/10.5204/mcj.1494.

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Introduction“Cage rage” is one of the most famous Internet memes (Figure 1) which made Nicolas Cage's stylised and sometimes excessive acting style very popular. His outbursts became a subject of many Youtube videos, supercuts (see for instance Hanrahan) and analyses, which turned his rage into a pop-cultural phenomenon. Cage’s outbursts of rage and (over)acting are, according to him (Freeman), inspired by German expressionism as in films like The Cabinet of Dr. Caligari (1920). How should this style of acting and its position within the context of the Hollywood industry today be read in socie

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