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Camouflage and mimicry have a long-standing tradition in military applications and have been largely employed from the 19th century onwards [1] — during World War I the concept of visual deception developed into an essential part of modern military tactics.
Fig. 1.
An example is presented in Figure 1.
References [1] P.
Rogers, Skin-integrated wireless haptic interfaces for virtual and augmented reality, Nature 575 (2019) 473–479

Subject Sequence ID Percentage of matches Alignment length E-value Frame direction GDVN01047171.1 83.12 3904 0 1 GDVN01047171.1 82.394 1278 0 1 *GDVN01045227.1 83.982 3677 0 1 GDVN01045226.1 82.884 3675 0 1 GDVN01010801.1 80.431 511 5.24E-131 1 GDVN01047170.1 80.655 336 3.10E-83 -1 GDVN01047170.1 83.206 262 7.80E-72 1 GDVN01047170.1 83.333 258 4.92E-68 1 GDVN01039324.1 79.006 362 1.61E-80 -1 GDVN01032094.1 84.375 224 3.79E-63 -1 GDVN01029078.1 82.353 221 2.24E-53 1 GDVN01023116.1 84.456 193 2.24E-53 -1 GDVN01049103.1 82.039 206 4.05E-50 1 GDVN01029670.1 85.185 162 3.79E-44 1 GDVN01009645.1 84.733 131 2.73E-33 1 GDVN01029342.1 90.741 108 9.52E-33 1 GDVN01014805.1 82.192 146 1.16E-31 -1 GDVN01011823.1 80.597 134 8.92E-27 1 GDVN01021683.1 84.762 105 1.61E-23 1 GDVN01019892.1 89.706 68 1.84E-16 1 GDVN01027555.1 72.785 158 2.73E-14 -1 GDVN01018348.1 75.969 129 1.16E-12 -1 GDVN01011241.1 78.788 99 4.05E-12 -1 GDVN01042689.1 84.058 69 6.01E-10 -1 GDVN01048619.1 90.476 42 1.09E-06 -1 Note: *GDVN01045227.1
The sequence with ID GDVN01047171.1 & GDVN01047170.1 is have 2 and 3 alignments respectively.
References [1] A.
Insects as Food & Feed, (2018) 1-8
Tang, Mitochondrial capture enriches mito‐DNA 100 fold, enabling PCR‐free mitogenomics biodiversity analysis, Molecular Ecology Resources. 16(2) (2016) 470-479

Table 1.
Fig. 1.
Results of cold bendability test performed on Zn-Cu-Ti sheets from various technological attempts Technological attempt Homogenized / Non-Homogenized Coil beginning Coil middle Coil end Average Bending angle 135° 180° 135° 180° 135° 180° #11 NH+ 1 2 0 1 2 1 1 1 2 1 1 0 1.1 #10 NH+ 1 1 0 1 2 2 1 1 2 2 2 1 1.3 #3 NH 2 2 1 1 1 2 0 1 2 2 1 1 1.3 #6 NH 1 2 0 2 2 2 1 1 1 2 0 2 1.3 #8 NH 1 2 1 1 2 2 2 1 1 2 0 2 1.4 #2 NH- 2 2 2 2 2 2 1 2 2 2 1 1 1.8 #1 NH- 2 2 1 2 2 2 2 2 2 2 2 2 1.9 #4 H 3 3 2 3 3 3 2 3 3 3 2 2 2.7 #7 H 3 3 2 2 3 3 3 3 3 3 2 3 2.8 #5 H 3 3 2 2 3 3 3 3 2 3 3 3 2.8 #9 H 3 3 3 3 3 3 3 3 2 3 2 3 2.8 Legend 3 2 1 0 Smooth surface "Orange peel" Visible seams Open cracks Important question are the differences between the homogenized and non-homogenized cast strip.
References [1] EN 988: Zinc and zinc alloys.
Gütegemeinschaft Bauelemente aus Titanzink [4] G.Boczkal, “Second phase morphology in the Zn-Ti0.1-Cu0.1 single crystals obtained at different growth rates”, Arch.of Met.and Mater., vol.57, iss.2, pp. 479-484, (2012) [5] G.Boczkal, “The influence of growth rate on mechanical and thermodynamical properties of the Zn-Ti0.075-Cu0.15 single crystals deformed at (0001)<11-20> system”, Materials Science Forum Vol. 674, pp 245-249,(2011) [6] G.Boczkal, B.Mikulowski, W.Wolczynski, “Oscillatory structure of The Zn-Cu-Ti single crystals”, Materials Science Forum Vol. 649, pp 113-118,(2010) [7] G.Boczkal, “Controlling the morphology and distribution of an intermetallic Zn16Ti phase in single crystals of Zn-Ti-Cu”, Chapter 7 in the book: “Modern Aspects of Bulk Crystal and Thin Film Preparation”, ed.

The concentration of A-Mo inhibitor was 200 mg·L-1, 400 mg·L-1, 600 mg·L-1 and 800 mg·L-1.
Table 1 shows the parameters obtained from Fig. 1.
Conclusion 1.
References [1] S.C.
Blasco-Tamarit, Cavitation-Corrosion Studies on Welded and Nonwelded Duplex Stainless Steel in Aqueous Lithium Bromide Solutions, Corrosion 63(5) (2007) 462-479

Fig.1 shows geometries and kinds of draw-bead which were analyzed.
Mechanical properties of the blank are summarized in Table 1.
Figure 4- Thickness distribution comparison through predefined path (left simulation, right experimental) Table 3- Design of experiments and results of objectives1 Rs h1 h2 d2 d5 d4 min sth thickness draw-in 10 1 1 3 1 3 3 0.521 54.96 9.7 20 1 1 1 1 1 3 0.543 50.83 8.3 30 2 1 2 2 1 3 0.541 65.96 6.9 40 1 1 3 3 2 3 0.539 72.36 15.3 50 3 3 2 1 1 2 0.522 71.83 6.9 60 3 1 1 3 1 3 0.544 64.58 8.4 70 1 1 3 1 3 3 0.521 54.96 9.7 80 3 3 3 3 1 3 0.53 88.16 8.3 90 3 1 3 1 3 3 0.502 69.33 8.5 100 1 1 1 3 1 3 0.551 54.57 9.1 Objective functions Thickness distribution.
References [1] M.
Jung, 1998, “Study of Dynamic explicit analysis in sheet metal forming processes using faster punch velocity and mass scaling scheme” Journal of material engineering and performance, Vol. 7 pp. 479-490

Table 1.
Ser., vol. 1, no.
Ii, pp. 569–574, 2018, doi: 10.1108/978-1-78756-793-1-00069
Ser., vol. 1, pp. 381–386, 2018, doi: 10.1108/978-1-78756-793-1-00087
Ser., vol. 1, pp. 479–486, 2018, doi: 10.1108/978-1-78756-793-1-00074

The chemical composition of the slag is shown in Table 1.
The experimental procedures are shown in Fig.1.
Reation /J·mol-1 Begin temperature/ K 8 3TiO2+C =Ti3O5+CO 273500-197.98T 1382 9 2Ti3O5+C = 3Ti2O3+CO 249500-152.47T 1637 10 Ti2O3+C =2TiO +CO 358500-195.67T 1833 11 TiO+C+ =Ti+CO 400200-159.87T 2504 12 1/5Ti3O5+8/5C=3/5TiC+CO 261740-162.346 T 1613 13 1/3Ti2O3+5/3C=2/3TiC+CO 263100-163.443T 1610 14 TiO+2C =TiC+CO 215400-147.33T 1462 15 1/2TiO2+3/2C=1/2TiC+CO 263700-168.285T 1567 16 1/2TiO2+C+1/4N2 =1/2TiN+CO 187950-127.925T 1470 17 1/2TiN+1/2C=1/2TiC+1/4N2 75750-40.36T 1877 When x = 0, the reaction(18) can be simplified as the reaction(15); When = 1, that can be simplified as the reaction(16).
References [1] LI wei, JIANG ming-xue, XIE bi-qiang, LU hong-xian.
Thermodynamic Data Notebook of Inorganics[M].Shenyang: Northeast University Press, 1993：449- 479 [8]Pangfusheng,Tang Aitao,Li Kui.Carbon nitrided titanium and composite materials reaction synthesis[M].Chongqing:Chongqing university press.2005 [9]Fang Min xian,Peng Jinhui,Chen Housheng,Chen Deming.A Thermodynamics-Based Analysis of Making Titanium Carbonitride Though Carbon Thermal Reduction[J].Journal of Kunming University of Science and Technology(Science and Technology).2006,31(6):6-12 [10]Li Xikun,Xiu zhimeng,Sun Xundong,Zheng Longxi.Synthesis of titanium carbonitride powders[J].Power Metallurgy industry,2004,14(1)：18-21

The chemical composition of fly ash is shown in Table 1 .
The pH of the mix was measured after 1 h.
The mix were stirred intermittently for 1 h and pH has measured after 1 hour .
N30 R30 7,12,15,18,20 30 70 10 28,28,28, 28,28 1,1,1,1,1 N40 R40 7,12,15,18,20 40 60 11 28,28,28, 28,28 1,1,1,1,1 N50 R50 7,12,15,18,20 50 50 12 28,28,28, 28,28 1,1,1,1,1 N70 R70 7,12,15,18,20 70 30 13 28,28,28, 28,28 1,1,1,1,1 % Initial lime Figure 1: Compressive strength(N/mm2) of mortar varying by initial lime percentage In normal temperature and raised one as one day and 28dayes Conclusions 1- The experiment elaborately portrayed that high raised curing temperatures specimen even in one day curing as R30 mortar (30%fly ash and 70% sand with varying lime 6 to 20 % at 80 degree Celsius steam curing ) in 1 day curing give 60 to 80 percent higher strengths than N30 specimen (normal temp with 30%fly ash and 70% sand with varying lime 6 to 20 % at 28 days normal curing ) , while, R70 specimens (70%fly ash and 30% sand with varying lime 6 to 20 % at 80 degree
Bulletin of the Association of Engineering Geologists, 4, 469-479

Experimental Table 1 Chemical composition of the alloys [wt. %] Alloy C Si B Cr Ni Targeted - 3.4 1.1 17.6 8.1 No.1 0.024 3.49 1.12 17.65 8.13 No.2 0.018 3.41 1.1 17.6 8.11 The targeted and actual compositions of the alloy are shown in Table 1.
In the as-casted microstructure of No.1 alloy (see Fig. 1(a)), there are a large number of massive, bar-shaped or granular secondary phases.
Fig. 1 (b) and (c) are the hot-rolled and heat-treated microstructures of the No. 1 alloy, respectively.
References [1] X Chen, H.
Heat Treat. 7-8(1988) 479-484

Fig. 1.
An originally proposed mathematical form of the area function is 128/1 8 4/1 3 2/1 2 1 2 0 c c c c c hC hChChChCA +++++= L , (3) where C0, C1, …, C8 are constants determined by curve fitting procedures [1].
References [1] W.C.
Prochazka: Thin Solid Films Vol. 476 (2005) 1
Bendavid: Thin Solid Films Vol. 479 (2005) 193