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Journal articles on the topic 'Aerospace material'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

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1

RAHIM, Erween, Takayuki OGAWA, Akihiko MIURA, Hiroyuki SASAHARA, Rei Koyasu, and Yasuhiro Yao. "3252 Ultrasonic Torsional Vibration Drilling of Aerospace Structure Material." Proceedings of International Conference on Leading Edge Manufacturing in 21st century : LEM21 2011.6 (2011): _3252–1_—_3252–4_. http://dx.doi.org/10.1299/jsmelem.2011.6._3252-1_.

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2

James, T. "Material ambitions [aerospace manufacturing]." Engineering & Technology 3, no. 11 (2008): 66–69. http://dx.doi.org/10.1049/et:20081109.

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3

Florin, PAVEL. "The World’s Aerospace Material Handbook." INCAS BULLETIN 2, no. 3 (2010): 129–30. http://dx.doi.org/10.13111/2066-8201.2010.2.3.14.

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4

Tejas Ajay, Baindur, Patil Mayur Vitthal, and G. Rajyalakshmi. "WEDM machining on Aerospace Materials for improving Material Properties." Materials Today: Proceedings 4, no. 8 (2017): 9107–16. http://dx.doi.org/10.1016/j.matpr.2017.07.266.

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5

Lee, Ho Sung, and Kookil No. "Materials and Manufacturing Technology for Aerospace Application." Key Engineering Materials 707 (September 2016): 148–53. http://dx.doi.org/10.4028/www.scientific.net/kem.707.148.

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This paper gives an overview of current work in materials and manufacturing technology for aerospace application. Finding the best material to use for a particular application is not simple and it depends on many factors including mission requirements like performance and safety, design requirements, strength to density ratio, operating temperature, and material technology prospects like current state of affordable materials/processes technologies. Materials with high specific strength have long been popular with the aerospace industry, as aerospace vehicle made from such materials provide the

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6

NIINO, Masayuki, and Yoshitsugu ISHIBASHI. "Development of new material for aerospace uses, "functionally gradient materials"." Journal of the Japan Welding Society 59, no. 6 (1990): 453–58. http://dx.doi.org/10.2207/qjjws1943.59.453.

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7

RABEEH, B., W. SOBOYEJO, and S. ROKHLIN. "AEROSPACE MATERIAL DAMAGE CHARACTERIZATION AND LIFE PREDICTIONS." International Conference on Aerospace Sciences and Aviation Technology 7, ASAT CONFERENCE (1997): 1–19. http://dx.doi.org/10.21608/asat.1997.25404.

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8

Ragauskas, Paulius, and Rimantas Belevičius. "IDENTIFICATION OF MATERIAL PROPERTIES OF COMPOSITE MATERIALS." Aviation 13, no. 4 (2009): 109–15. http://dx.doi.org/10.3846/1648-7788.2009.13.109-115.

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Present paper describes the facilities of composite material properties identification technique using specimen vibration tests, genetic algorithms, finite elements analysis and specimen shape optimization. In identification process the elastic constants in a numerical model is updated so that the output from the numerical code fits the results from vibration testing. Main problem analysed in this paper is that Poisson's ratio is the worst determined elastic characteristic due to its low influence on specimen eigenfrequencies. It is shown that it is possible to increase its influence by choosi

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9

Sun, De Ying. "Research the Utilization Rate of Aluminum Alloy Material." Applied Mechanics and Materials 595 (July 2014): 79–82. http://dx.doi.org/10.4028/www.scientific.net/amm.595.79.

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There are many parts in aerospace fixing device, the 7075 - t351 brand aluminum alloy is a commonly used material of these parts [2].The material has high strength, good toughness, wear resistance and resistance to spalling corrosion resistance and other characteristics; After the machining deformation, comprehensive mechanical processing performance is good [1]. As a result, the materials are widely used in aerospace equipment. Smaller wall thickness, complex structure, multiple azimuth need processing, is the characteristics of these parts, make the individual parts machining material consum

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10

Sanoj, P., and Balasubramanian Kandasubramanian. "Hybrid Carbon-Carbon Ablative Composites for Thermal Protection in Aerospace." Journal of Composites 2014 (March 6, 2014): 1–15. http://dx.doi.org/10.1155/2014/825607.

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Composite materials have been steadily substituting metals and alloys due to their better thermomechanical properties. The successful application of composite materials for high temperature zones in aerospace applications has resulted in extensive exploration of cost effective ablative materials. High temperature heat shielding to body, be it external or internal, has become essential in the space vehicles. The heat shielding primarily protects the substrate material from external kinetic heating and the internal insulation protects the subsystems and helps to keep coefficient of thermal expan

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Budiman, Arie Yudha, and Amrifan Saladin Mohruni. "A REVIEW ON THIN WALLED CRYOGENIC MACHINING ON INCONEL OR AEROSPACE MATERIALS." Journal of Mechanical Science and Engineering 7, no. 1 (2020): 001–5. http://dx.doi.org/10.36706/jmse.v7i1.34.

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Cutting fluids are widely used in machining processes throughout the world. However, this cutting liquid is the source of many environmental pollution problems. In order to reduce or eliminate the effect produced by cutting fluids, it is necessary to switch to a continuous machining technique such as using small amounts of cutting fluid, liquid nitrogen, vegetable oil or compressed air as a cooling lubrication medium. Cryogenic coolant is found to be more efficient, economical, cost-effective and environmentally friendly when compared to the conventional coolant, especially in mass production.

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12

Silva, José M., Tessaleno C. Devezas, A. Silva, L. Gil, C. Nunes, and N. Franco. "Exploring the Use of Cork Based Composites for Aerospace Applications." Materials Science Forum 636-637 (January 2010): 260–65. http://dx.doi.org/10.4028/www.scientific.net/msf.636-637.260.

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Aerospace components are characterized by having high strength to weight ratios in order to obtain lightweight structures. Recently, different types of sandwich components using composite materials have been developed with the purpose of combining the effect of reinforced face-sheets with low weight core materials, such as honeycombs and foams. However, these materials must combine damage tolerance characteristics with high resistance under both static and dynamic loads. Cork composites can be considered as an alternative material for sandwich components since cork is a natural material with s

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13

Silva, J. M., C. Z. Nunes, N. Franco, and P. V. Gamboa. "Damage tolerant cork based composites for aerospace applications." Aeronautical Journal 115, no. 1171 (2011): 567–75. http://dx.doi.org/10.1017/s0001924000006205.

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Abstract This work aims at improving the resilience and damage tolerant properties of CFRP by using cork, which is a natural material with good energy absorption capacity and thermal insulating and vibration damping characteristics. Two types of materials were considered: a sandwich formed by carbon-epoxy facesheets with a cork-epoxy core and a carbon-epoxy laminate with embedded cork granulates. The damage tolerant properties were evaluated by low velocity impact tests according to the type of material. Additionally, this work intends to evaluate the feasibility of using a cork agglomerate co

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14

Wang, Yi Wen, Ming Na Ding, Wen Juan Zheng, Zhen Chen, and Jing Shu Hu. "Design of Typical Aerospace Materials Database System." Materials Science Forum 800-801 (July 2014): 644–48. http://dx.doi.org/10.4028/www.scientific.net/msf.800-801.644.

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Due to the rapid development of aerospace industry, the amount of cutting data is increasing. Establishing cutting database for aerospace industry is necessary. Therefore, this article designs the typical aerospace material database system. According to project requirements analysis and the conceptual design, nine function blocks is set. They are data management, experiment management, optimization management, cutting tool design, cutting tool simulation, knowledge base, aerospace solutions, systems management, and help. And the article describes content and processes of every function block.

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15

Sellitto, Andrea, Aniello Riccio, A. Russo, Antonio Garofano, and Mauro Zarrelli. "Nanofillers’ Effects on Fracture Energy in Composite Aerospace Structures." Key Engineering Materials 827 (December 2019): 43–48. http://dx.doi.org/10.4028/www.scientific.net/kem.827.43.

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Composite materials damage behaviour is, nowadays, extensively investigated in the frame of aerospace research programmes. Among the several failure mechanisms which can affect composites, delamination can be considered as the most critical one, especially when combined to compressive loading conditions. In this context, nanofillers can represent an effective way to increase the composites fracture toughness with a consequent reduction of the delamination onset and evolution. Hence, in this paper, the toughening effect of the nanofillers on the delamination growth in composite material panels,

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16

Han, X., and G. R. Liu. "Computational Inverse Technique for Material Characterization of Functionally Graded Materials." AIAA Journal 41, no. 2 (2003): 288–95. http://dx.doi.org/10.2514/2.1942.

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17

Das, D. K., and Jit Sarkar. "Graphene–magnesium nanocomposite: An advanced material for aerospace application." Modern Physics Letters B 32, no. 06 (2018): 1850075. http://dx.doi.org/10.1142/s0217984918500756.

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This work focuses on the analytical study of mechanical and thermal properties of a nanocomposite that can be obtained by reinforcing graphene in magnesium. The estimated mechanical and thermal properties of graphene–magnesium nanocomposite are much higher than magnesium and other existing alloys used in aerospace materials. We also altered the weight percentage of graphene in the composite and observed mechanical and thermal properties of the composite increase with increase in concentration of graphene reinforcement. The Young’s modulus and thermal conductivity of graphene–magnesium nanocomp

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18

Corcoran, A., L. Sexton, B. Seaman, P. Ryan, and G. Byrne. "The laser drilling of multi-layer aerospace material systems." Journal of Materials Processing Technology 123, no. 1 (2002): 100–106. http://dx.doi.org/10.1016/s0924-0136(01)01123-2.

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19

Min, Liyi, Qiwen Liu, and Lisheng Liu. "Crack Growth Simulation of Functionally Graded Materials Based on Improved Bond-Based Peridynamic Model." Materials 14, no. 11 (2021): 3032. http://dx.doi.org/10.3390/ma14113032.

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Functionally graded materials (FGMs) are widely used in the aerospace industry, especially for the thermal protection shields of aerospace vehicles. Studies show that the initiation and expansion of micro-cracks are important factors that adversely affect the service life of these shields. Based on the peridynamic theory of bonds, an improved peridynamic model is proposed in the present study for FGMs. In the proposed model, integral equivalence is applied to calculate the required material parameters. Obtained results reveal that this method can better reflect the gradient change of material

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20

Katz-Demyanetz, Alexander, Vladimir V. Popov, Aleksey Kovalevsky, Daniel Safranchik, and Andrey Koptyug. "Powder-bed additive manufacturing for aerospace application: Techniques, metallic and metal/ceramic composite materials and trends." Manufacturing Review 6 (2019): 5. http://dx.doi.org/10.1051/mfreview/2019003.

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The current paper is devoted to classification of powder-bed additive manufacturing (PB-AM) techniques and description of specific features, advantages and limitation of different PB-AM techniques in aerospace applications. The common principle of “powder-bed” means that the used feedstock material is a powder, which forms “bed-like” platform of homogeneous layer that is fused according to cross-section of the manufactured object. After that, a new powder layer is distributed with the same thickness and the “printing” process continues. This approach is used in selective laser sintering/meltin

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21

Liang, Jian Xun, and Yun Tao Cai. "Application of Advanced Carbon Fiber Composite Material in Sport Equipments." Applied Mechanics and Materials 217-219 (November 2012): 63–66. http://dx.doi.org/10.4028/www.scientific.net/amm.217-219.63.

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Advanced composite material not only is widely applied in aerospace, automobile and other industry fields, but also is one of the best materials for developing sport equipments. This paper introduces the advantages of carbon fiber composite material application in sport equipments and clarifies that application of this kind of high-tech material in sport equipments can greatly improve sport achievement by use of typical examples. Carbon fiber composite material has become one of essential novel materials for developing modern sport equipments.

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22

Wu, Chun, Wen Xin Ma, Ya Ping Chen, Ying Li, Yan Chen, and Jing Li. "Nano Materials and its Application in Space." Applied Mechanics and Materials 482 (December 2013): 34–37. http://dx.doi.org/10.4028/www.scientific.net/amm.482.34.

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Nano material is a new type of multi-functional materials, this article simply introduces the development present situation, performance and preparation method, and application in the aerospace field.

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23

Lv, Jia Hui, Wei Ze Wang, Shan Tung Tu, and Shao Wu Liu. "Failure Cases Analysis in Aerospace Field." Materials Science Forum 993 (May 2020): 1277–85. http://dx.doi.org/10.4028/www.scientific.net/msf.993.1277.

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The major concern in the aviation industry is the flight safety. Although great effort has been put into the development of material and system reliability, the failure cases of fatal accidents still occur nowadays. Due to the complexity of the aviation system and the interaction among the failure components, it is difficult to do the failure analysis of the related equipment. This study focused on surveying the failure cases in aviation, which were extracted from failure analysis journals, including Engineering Failure Analysis and Case studies in Engineering Failure Analysis, in order to obt

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24

Umanath, K., S. T. Selvamani, K. Palanikumar, and T. Raphael. "Effect of Hardness on the Wear Behavior of Hybrid Metal Matrix Composites." Advanced Materials Research 984-985 (July 2014): 536–40. http://dx.doi.org/10.4028/www.scientific.net/amr.984-985.536.

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Aerospace industry and automobile industries are enhanced performance necessary for materials with better qualities compare to conservative materials. In automotive areas, this is predominantly factual for power train employed as conflicting to body application. For each kind of appliance, description such as hardness of the material, wear resistance, temperature withstands ability, plasticity, fracture, fatigue strength, etc. It must be as high as possible, while parameters such as density and cost must be minimized; the latter is of general concern for automobile use and relatively inexpensi

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25

Lee, Jae Hoon, Bum Soo Yoon, Ji-Won Park, Gunho Song, and Kwang Joon Yoon. "Flexural Deflection Prediction of Piezo-Composite Unimorph Actuator Using Material Orthotropy and Nonlinearity of Piezoelectric Material Layer." Coatings 10, no. 5 (2020): 437. http://dx.doi.org/10.3390/coatings10050437.

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Layered piezo-composite unimorph actuators have been studied by many research teams to provide active vibration control of thin-walled aerospace structures, control the shapes of aircraft wing airfoils, and control the fins of small missiles, because they require less space and provide better frequency responses than conventional electro-magnetic motor actuator systems. However, due to the limited actuation strains of conventional piezo-composite unimorph actuators with poly-crystalline piezoelectric ceramic layers, they have not been implemented effectively as actuators for small aerospace ve

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26

Dassios, Konstantinos G., Evangelos Z. Kordatos, Dimitrios G. Aggelis, and Theodore E. Matikas. "Nondestructive Damage Evaluation in Ceramic Matrix Composites for Aerospace Applications." Scientific World Journal 2013 (2013): 1–12. http://dx.doi.org/10.1155/2013/715945.

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Infrared thermography (IRT) and acoustic emission (AE) are the two major nondestructive methodologies for evaluating damage in ceramic matrix composites (CMCs) for aerospace applications. The two techniques are applied herein to assess and monitor damage formation and evolution in a SiC-fiber reinforced CMC loaded under cyclic and fatigue loading. The paper explains how IRT and AE can be used for the assessment of the material’s performance under fatigue. IRT and AE parameters are specifically used for the characterization of the complex damage mechanisms that occur during CMC fracture, and th

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27

Goyal, Ashish, Anand Pandey, and Pooja Sharma. "Machinability of Inconel 625 Aerospace Material Using Cryogenically Treated WEDM." Solid State Phenomena 266 (October 2017): 38–42. http://dx.doi.org/10.4028/www.scientific.net/ssp.266.38.

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Machinability of aerospace material, Inconel 625 through Wire cut electrical discharge machining has been performed and compared using Taguchi’s Orthogonal L18 (21*35). Normal diffused and cryogenic treated diffused wires are being used as a tool electrode to investigate the effects of machining parameters viz. tool electrode, peak current, pulse on time, pulse off time, wire feed and wire tension on the response MRR. The present study resulted that cryogenic treated tool electrode give better performance in comparison to normal wire electrode assisting in improving stock removal and less elec

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28

Li Jing, 李静, 郑轶 Zheng Yi, 罗晋 Luo Jin, 陈松林 Chen Songlin, 关振威 Guan Zhenwei, and 梁璐 Liang Lu. "Laser ablation effect of composite coating applied to aerospace material." High Power Laser and Particle Beams 26, no. 2 (2014): 29003. http://dx.doi.org/10.3788/hplpb20142602.29003.

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29

ITOH, Koji. "Development of new material for aerospace uses "heat resistant composites"." Journal of the Japan Welding Society 59, no. 6 (1990): 446–52. http://dx.doi.org/10.2207/qjjws1943.59.446.

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30

Alderliesten, R. C. "Designing for damage tolerance in aerospace: A hybrid material technology." Materials & Design 66 (February 2015): 421–28. http://dx.doi.org/10.1016/j.matdes.2014.06.068.

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31

Liu, Ping, Roger M. Groves, and Rinze Benedictus. "Signal processing in optical coherence tomography for aerospace material characterization." Optical Engineering 52, no. 3 (2013): 033201. http://dx.doi.org/10.1117/1.oe.52.3.033201.

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32

Holmes, Mark. "Synthetic diamond composite tooling material provides step change in aerospace." Reinforced Plastics 59, no. 6 (2015): 291–93. http://dx.doi.org/10.1016/j.repl.2014.12.069.

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33

Zhang, Yanzhong, and Xiaohua Huang. "Simulation and Research of Aerospace Material Milling Based On ABAQUS." Journal of Physics: Conference Series 1653 (October 2020): 012070. http://dx.doi.org/10.1088/1742-6596/1653/1/012070.

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34

Thomson, J., R. Zavadil, M. Sahoo, A. Dadouche, W. Dmochowski, and M. Conlon. "Development of a Lead-Free Bearing Material for Aerospace Applications." International Journal of Metalcasting 4, no. 1 (2010): 19–30. http://dx.doi.org/10.1007/bf03355483.

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35

Bhasha, Sanjeev Gautam, Parul Malik, and Purnima Jain. "Ceramic Composites for Aerospace Applications." Diffusion Foundations 23 (August 2019): 31–39. http://dx.doi.org/10.4028/www.scientific.net/df.23.31.

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Ceramic composites is playing crucial role to accomplish highly efficiently and cost effective equipment for aerospace industry. The instigation of ceramics into aircraft industry is a promising step towards virtuous future. Ceramics has a key role in innovation of highly competent material for space travel which is highly economical and environmentally sustainable. Advancement in making fuel efficient engines are necessity in present scenario due to the harmful emissions releases in the environment by burning of fuel to power up engine. The high temperature application of composites makes it

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36

Wang, Le Xin, Zhi Min Zhao, and Xu Fang Jia. "Experimental Study of Light-Repair on Composite Material Deflection." Advanced Materials Research 233-235 (May 2011): 2072–76. http://dx.doi.org/10.4028/www.scientific.net/amr.233-235.2072.

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Composites, as a type of new material with typical characteristics, has been applied in aerospace, space, buildings, bridges and many other areas. Rapid repair from damaged composites has become a hot research project. This paper proposed a technique of light repair on composites, which is often used as specimen in aerospace composites. The research has taken advantage of modern optical measurement to study the influence of light remediation on the structural bending of composites, put forth a law of deflection variation, and proven that light remediation is feasible. The result of this resear

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37

Roux, Maxime, Nicolas Eguémann, Clemens Dransfeld, Frédéric Thiébaud, and Dominique Perreux. "Thermoplastic carbon fibre-reinforced polymer recycling with electrodynamical fragmentation." Journal of Thermoplastic Composite Materials 30, no. 3 (2016): 381–403. http://dx.doi.org/10.1177/0892705715599431.

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The end of life of carbon fibre-reinforced polymer (CFRP) structures represents a major challenge to the aerospace industry, as new European regulations are demanding recycling solutions that can be complicated and expensive to apply. This study aims to address new practical ways to recycle CFRP materials. CFRP materials with a polyether ether ketone (PEEK) matrix were fragmented via electrodynamical fragmentation, which exhibits several benefits compared to mechanical shredding processes, especially for composites commonly found in the aerospace industry. The fragments are characterized and r

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38

Chen, Yan Yan. "The Application of Carbon Fiber Materials in Sports Equipment." Applied Mechanics and Materials 687-691 (November 2014): 4240–43. http://dx.doi.org/10.4028/www.scientific.net/amm.687-691.4240.

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Carbon fiber materials are not only widely used in aerospace, automotive and other industries, but also develop one of the best sports equipment selection. Elaborated by typical examples, this paper introduces the carbon fiber material used in the game of high-tech equipment and indicates that this material greatly promoted the improvement of sports performance. Carbon fiber materials have become one of the new materials which are essential for the development of modern sports equipment.

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39

Rihakova, L., and H. Chmelickova. "Laser Micromachining of Glass, Silicon, and Ceramics." Advances in Materials Science and Engineering 2015 (2015): 1–6. http://dx.doi.org/10.1155/2015/584952.

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A brief review is focused on laser micromachining of materials. Micromachining of materials is highly widespread method used in many industries, including semiconductors, electronic, medical, and automotive industries, communication, and aerospace. This method is a promising tool for material processing with micron and submicron resolution. In this paper micromachining of glass, silicon, and ceramics is considered. Interaction of these materials with laser radiation and recent research held on laser material treatment is provided.

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Gasson, Peter C. "Aerospace Materials and Material Technologies Vol 2: Aerospace Material TechnologiesEdited by N. E. Prasad and R. J. H. Wanhill Springer, 2017. xxviii; 557pp. Illustrated. £149.99. ISBN 978-981-10-2142-8." Aeronautical Journal 122, no. 1258 (2018): 2039–43. http://dx.doi.org/10.1017/aer.2018.132.

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Morgeneyer, T. F., Marco J. Starink, and I. Sinclair. "Experimental Analysis of Toughness in 6156 Al-Alloy Sheet for Aerospace Applications." Materials Science Forum 519-521 (July 2006): 1023–28. http://dx.doi.org/10.4028/www.scientific.net/msf.519-521.1023.

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Analysis of toughness in 6156 Al-Mg-Si-Cu sheet has been performed using enhanced Kahn tear tests on samples quenched at different rates, whilst microstructures of the samples have been assessed using differential scanning calorimetry, scanning electron microscopy and transmission electron microscopy. Crack initiation energies were unaffected by changing water quench temperature from 20°C to 60°C, however a significant reduction was evident on air cooling. Crack propagation resistance was reduced for both 60°C water quenched and air cooled materials. The failure morphology of the air cooled ma

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42

M., Arun, Muthukumaran M., and Balasubramanian S. "Tribological characterization of friction stir welded dissimilar aluminum alloy AA6061–AA5083 reinforced with CeO2 and La2O3 nanoparticles." Industrial Lubrication and Tribology 73, no. 5 (2021): 783–88. http://dx.doi.org/10.1108/ilt-01-2021-0009.

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Purpose Dissimilar materials found applications in the structural fields to withstand the different types of loads and provide multi-facet properties to the final structure. Aluminum alloy materials are mostly used in aerospace and marine industries to provide better strength and safeguard the material from severe environmental conditions. The purpose of this study is to develop new material with superior strength to challenge the severe environmental conditions. Design/methodology/approach In the present investigation, friction stir welding (FSW) dissimilar joints were prepared from AA6061 an

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43

Li, Jeremy Zheng. "Computational Simulation and Prototype Testing of Nanocoating on Products in Aerospace Industry." Advanced Materials Research 750-752 (August 2013): 2088–91. http://dx.doi.org/10.4028/www.scientific.net/amr.750-752.2088.

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The material damages in aerospace industry caused by correction can be detected in many different products including welded and bolted areas in aircraft and jet engines. The corrosion occurs when different conducted materials contact to each other in electrolyte media and different conducted materials present potential difference that causes rusting. The rusting problems in products lead both safety issues and billions of dollar loss in different businesses including aerospace industry. This paper studies the rusting mechanism and anti-corrosive coatings by applying computational simulation an

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44

Kinawy, Moustafa, Richard Butler, and Giles W. Hunt. "Bending strength of delaminated aerospace composites." Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences 370, no. 1965 (2012): 1780–97. http://dx.doi.org/10.1098/rsta.2011.0337.

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Buckling-driven delamination is considered among the most critical failure modes in composite laminates. This paper examines the propagation of delaminations in a beam under pure bending. A pre-developed analytical model to predict the critical buckling moment of a thin sub-laminate is extended to account for propagation prediction, using mixed-mode fracture analysis. Fractography analysis is performed to distinguish between mode I and mode II contributions to the final failure of specimens. Comparison between experimental results and analysis shows agreement to within 5 per cent in static pro

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Brandt, Milan, Shou Jin Sun, Martin Leary, S. Feih, J. Elambasseril, and Qian Chu Liu. "High-Value SLM Aerospace Components: From Design to Manufacture." Advanced Materials Research 633 (January 2013): 135–47. http://dx.doi.org/10.4028/www.scientific.net/amr.633.135.

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Today additive manufacturing is shaping the future of global manufacturing and is influencing the design and manufacturability of tomorrows products. With selective laser melting (SLM), parts can be built directly from computer models or from measurements of existing components to be re-engineered, and therefore bypass traditional manufacturing processes such as cutting, milling and grinding. Benefits include: 1) new designs not possible using conventional subtractive technology, 2) dramatic savings in time, materials, wastage, energy and other costs in producing new components, 3) significant

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Zhao, Ning, Peng Yuan Qiu, and Lei Lei Cao. "Development and Application of Functionally Graded Material." Advanced Materials Research 562-564 (August 2012): 371–75. http://dx.doi.org/10.4028/www.scientific.net/amr.562-564.371.

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Functionally graded material is a new kind of inhomogeneous material whose material properties change continuously with spatial positions. As a result of its excellent performance, it’s widely used in aerospace, nuclear engineering, biomedicine and some other fields that requirement of material is very strict. Classification based on different applications and research actuality are shown in this article.

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Gomez-Gallegos, Ares, Paranjayee Mandal, Diego Gonzalez, Nicola Zuelli, and Paul Blackwell. "Studies on Titanium Alloys for Aerospace Application." Defect and Diffusion Forum 385 (July 2018): 419–23. http://dx.doi.org/10.4028/www.scientific.net/ddf.385.419.

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Since the development of the Ti54M titanium alloy in 2003, its application within the aerospace sector has gradually increased due to the combination of properties such as improved forgeability and machinability, low flow stress at elevated temperatures, and superplastic characteristics. However, for the successful exploitation of Ti54M a comprehensive understanding of its mechanical characteristics, microstructure stability, and superplastic behaviour is required. The superplastic forming of titanium alloys is characterised by high deformation at slow strain rates and high temperatures which

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Uzgur, Sinem Cevik, Yagiz Uzunonat, S. Fehmi Diltemiz, Melih Cemal Kushan, and Rabia Gunay. "State-of-Art Technology ALLVAC 718 Plus Superalloy for Gas Turbine Engine Parts." Advanced Materials Research 213 (February 2011): 131–35. http://dx.doi.org/10.4028/www.scientific.net/amr.213.131.

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Innovations on the aerospace and aircraft industry have been throwing light upon building to future’s engineering architecture at the today’s globalization world where technology is the indispensable part of life. On the basis of aviation sector, the improvements of materials used in aircraft gas turbine engines which constitute 50 % of total aircraft weight must protect its actuality continuously. Utilization of super alloys in aerospace and defense industries can not be ignored because of excellent corrosion and oxidation resistance, high strength and long creep life at elevated temperatures

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Saboori, Mehdi, Javad Gholipour, Henri Champliaud, Augustin Gakwaya, Jean Savoie, and Priti Wanjara. "Effect of Material Model on Finite Element Modeling of Aerospace Alloys." Key Engineering Materials 554-557 (June 2013): 151–56. http://dx.doi.org/10.4028/www.scientific.net/kem.554-557.151.

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Increasing acceptance and use of hydroforming technology within the aerospace industry requires a comprehensive understanding of critical issues such as the material characteristics, friction condition and hydroformability of the material. Moreover, the cost of experiments that can be reduced by accurate finite element modeling (FEM), which entails the application of adapted constitutive laws for reproducing with confidence the material behavior. In this paper, the effect of different constitutive laws on FEM of tubular shapes is presented. The free expansion process was considered for develop

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Poojari, Yajnesh M., Koustubh S. Annigeri, Nilesh Bandekar, et al. "An alternative coating material for gas turbine blade for aerospace applications." Journal of Physics: Conference Series 1706 (December 2020): 012183. http://dx.doi.org/10.1088/1742-6596/1706/1/012183.

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