| Literature DB >> 35345398 |
Temesgen Abriham Miliket1,2, Mesfin Belayneh Ageze3, Muluken Temesgen Tigabu1,4, Migbar Assefa Zeleke5,6.
Abstract
Performances of hybrid Natural Fiber-Reinforced Composites (NFRCs) from E-glass, Nacha (Hibiscus macranthus Hochst. Ex-A. Rich.), and Sisal (Agave sisalana) fibers are investigated for wind turbine blades applications. The process of composite manufacturing was getting started with harvesting and extracting the fibers from undesired constituents. To improve the interfacial interaction between fibers, it was further treated with 5% of NaOH and remnants removal. The experiment was performed based on the Taguchi method, specifically with L16 orthogonal array. Four levels of a natural fiber weight ratio (i.e. 5%, 10%, 15 %, and 20%) were considered during the composite preparations process while the weight of glass fiber was maintained at 5% and 10%. The composites are manufactured using the hand lay-up method, and the test specimens are as per American Society for Testing and Materials (ASTM) standards. Then, tensile, compressive, and flexural tests were carried out using a universal testing machine (UTM). Analysis of variance (ANOVA) was employed to determine the factors which affect the experimental responses. Hence, in the main effect, it was confirmed that Nacha fiber (%wt of N) significantly contributes to tensile, compressive, and flexural strength at a 95% level of confidence. Furthermore, the optimal fiber compositions of composites are determined based on a higher signal-to-noise ratio (S/N) for the corresponding strengths.Entities:
Keywords: ANOVA; Biodegradable; Natural fiber-reinforced composite material; Taguchi methods; Wind turbine blade materials
Year: 2022 PMID: 35345398 PMCID: PMC8956877 DOI: 10.1016/j.heliyon.2022.e09092
Source DB: PubMed Journal: Heliyon ISSN: 2405-8440
Figure 1Plants were used for the study, (a) Nacha (b) Sisal.
Figure 2Working methodology.
Physical and mechanical properties of individual fibers.
| Material | Density (g/cm3) | Moisture content (%) | Elongation at Break (%) | Ref. |
|---|---|---|---|---|
| Nacha fiber | 1.38–1.43 | 7.8–12.46 | 1.4 | [ |
| Sisal fiber | 1.2 | 5–6 | 8 | [ |
| Glass fiber | 2.5 | - | 0.5 | [ |
Figure 3Composite manufacturing process.
Specimen preparation standard.
| Test type | Specimen Standard | Dimensions (mm) |
|---|---|---|
| Tensile | ASTM D 3039 [ | 165 × 19 × 2 |
| Flexural strength | ASTM D 790 [ | 126 × 12.5 × 2 |
| Compressive | ASTM D 3410 [ | 37.5 × 16.5 × 3 |
Levels of control factors used in the experiment.
| Levels | %wt of G | % wt of N | % of S |
|---|---|---|---|
| 1 | 5 | 5 | 5 |
| 2 | 10 | 10 | 10 |
| 3 | 10 | 15 | 15 |
| 4 | 10 | 20 | 20 |
Figure 4ASTM standard composites specimens (a) tensile; (b) flexural; (c) compressive.
Figure 5Experimental setups (a) Tensile; (b) Flexural; (c) Compressive.
Experimental results of tensile strength with a corresponding S/N ratio.
| Experiments | %wt of G | %wt of N | %wt of S | Tensile load (kN) | Tensile stress (MPa) | S/N |
|---|---|---|---|---|---|---|
| 1 | 1 | 1 | 1 | 9.4 | 167.857 | 22.45926 |
| 2 | 1 | 2 | 2 | 11.82 | 207.22 | 24.44905 |
| 3 | 1 | 3 | 3 | 10.16 | 181.429 | 23.13458 |
| 4 | 1 | 4 | 4 | 11.2 | 200 | 23.98106 |
| 5 | 2 | 1 | 2 | 10.78 | 192.5 | 23.64908 |
| 6 | 2 | 2 | 1 | 11 | 196.429 | 23.82456 |
| 7 | 2 | 3 | 4 | 10.26 | 183.214 | 23.21965 |
| 8 | 2 | 4 | 3 | 9.76 | 174.286 | 22.7857 |
| 9 | 3 | 1 | 3 | 10.86 | 193.929 | 23.7133 |
| 10 | 3 | 2 | 4 | 12.58 | 220.12 | 24.99031 |
| 11 | 3 | 3 | 1 | 10.26 | 183.214 | 23.21965 |
| 12 | 3 | 4 | 2 | 12.34 | 216.26 | 24.823 |
| 13 | 4 | 1 | 4 | 10.24 | 182.857 | 23.2027 |
| 14 | 4 | 2 | 3 | 11.54 | 206.071 | 24.24082 |
| 15 | 4 | 3 | 2 | 11.22 | 195.44 | 23.99656 |
| 16 | 4 | 4 | 1 | 11.38 | 203.214 | 24.11955 |
Experimental results of flexural strength with a corresponding S/N ratio.
| Experiments | %wt of G | %wt of N | %wt of S | Flexural load (kN) | Flexural stress (MPa) | S/N |
|---|---|---|---|---|---|---|
| 1 | 1 | 1 | 1 | 12.16 | 217.143 | 24.69537 |
| 2 | 1 | 2 | 2 | 11.82 | 211.071 | 24.44905 |
| 3 | 1 | 3 | 3 | 11.76 | 210 | 24.40485 |
| 4 | 1 | 4 | 4 | 9.88 | 176.429 | 22.89184 |
| 5 | 2 | 1 | 2 | 12.24 | 205.87 | 24.72271 |
| 6 | 2 | 2 | 1 | 10.76 | 107.6 | 23.60333 |
| 7 | 2 | 3 | 4 | 11.32 | 113.2 | 24.04401 |
| 8 | 2 | 4 | 3 | 11.78 | 117.8 | 24.38999 |
| 9 | 3 | 1 | 3 | 12.48 | 210.43 | 24.89138 |
| 10 | 3 | 2 | 4 | 11.14 | 111.4 | 23.90479 |
| 11 | 3 | 3 | 1 | 11.5 | 115 | 24.18104 |
| 12 | 3 | 4 | 2 | 12.1 | 201.19 | 24.62279 |
| 13 | 4 | 1 | 4 | 12.02 | 192.70 | 24.59479 |
| 14 | 4 | 2 | 3 | 11.86 | 211.786 | 24.4784 |
| 15 | 4 | 3 | 2 | 11.94 | 213.214 | 24.53679 |
| 16 | 4 | 4 | 1 | 9.56 | 195.6 | 22.57624 |
Experimental results of compressive strength with a corresponding S/N ratio.
| Experiments | %wt of G | %wt of N | %wt of S | Compressive load (kN) | Compressive stress (MPa) | S/N |
|---|---|---|---|---|---|---|
| 1 | 1 | 1 | 1 | 12.04 | 267.556 | 24.61404 |
| 2 | 1 | 2 | 2 | 14.16 | 308.55 | 26.02278 |
| 3 | 1 | 3 | 3 | 12.74 | 283.111 | 25.1049 |
| 4 | 1 | 4 | 4 | 12.48 | 277.333 | 24.92581 |
| 5 | 2 | 1 | 2 | 11.72 | 260.444 | 24.38007 |
| 6 | 2 | 2 | 1 | 12.8 | 290.444 | 25.14607 |
| 7 | 2 | 3 | 4 | 12.52 | 278.222 | 24.9536 |
| 8 | 2 | 4 | 3 | 12 | 266.667 | 24.58514 |
| 9 | 3 | 1 | 3 | 10.36 | 230.222 | 23.30871 |
| 10 | 3 | 2 | 4 | 13.52 | 300.444 | 25.62105 |
| 11 | 3 | 3 | 1 | 13.9 | 291.37 | 25.86181 |
| 12 | 3 | 4 | 2 | 10.54 | 255.5 | 23.45973 |
| 13 | 4 | 1 | 4 | 10.86 | 289.47 | 23.72076 |
| 14 | 4 | 2 | 3 | 13.84 | 241.333 | 25.81876 |
| 15 | 4 | 3 | 2 | 13.74 | 307.556 | 25.76138 |
| 16 | 4 | 4 | 1 | 10.86 | 235.00 | 23.72141 |
ANOVA for S/N ratios for tensile strength.
| Source | DF | Seq SS | Adj SS | Adj MS | F | P |
|---|---|---|---|---|---|---|
| %wt of G | 3 | 1.6549 | 1.6549 | 0.5516 | 3.52 | 0.089 |
| %wt of N | 3 | 3.1787 | 3.1787 | 1.0596 | 6.75 | 0.024 |
| %wt of S | 3 | 1.7466 | 1.7466 | 0.5822 | 3.71 | 0.081 |
| Residual Error | 6 | 0.9414 | 0.9414 | 0.1569 | ||
| Total | 15 | 7.5216 |
ANOVA for S/N ratios flexural strength.
| Source | DF | Seq SS | Adj SS | Adj MS | F | P |
|---|---|---|---|---|---|---|
| %wt of G | 3 | 0.284 | 0.284 | 0.09465 | 0.41 | 0.755 |
| %wt of N | 3 | 2.5156 | 2.5156 | 0.83852 | 3.59 | 0.086 |
| %wt of S | 3 | 2.2749 | 2.2749 | 0.75829 | 3.25 | 0.102 |
| Residual Error | 6 | 1.4008 | 1.4008 | 0.23346 | ||
| Total | 15 | 6.4752 |
ANOVA for S/N ratios for compressive strength.
| Source | DF | Seq SS | Adj SS | Adj MS | F | P |
|---|---|---|---|---|---|---|
| %wt of G | 3 | 0.7732 | 0.77323 | 0.25774 | 0.57 | 0.656 |
| %wt of N | 3 | 8.5366 | 8.53661 | 2.84554 | 6.28 | 0.028 |
| %wt of S | 3 | 0.0841 | 0.0841 | 0.02803 | 0.06 | 0.978 |
| Residual Error | 6 | 2.7199 | 2.71991 | 0.45332 | ||
| Total | 15 | 12.1139 |
Response table for S/N ratios for tensile strength.
| Larger is better | |||
|---|---|---|---|
| Level | %wt of G | %wt of N | %wt of S |
| 1 | 23.51 | 23.26 | 23.41 |
| 2 | 23.37 | 24.38 | 24.23 |
| 3 | 24.19 | 23.39 | 23.47 |
| 4 | 23.89 | 23.93 | 23.85 |
| Delta | 0.82 | 1.12 | 0.82 |
| Rank | 3 | 1 | 2 |
Response table for S/N ratios for flexural strength.
| Larger is better | |||
|---|---|---|---|
| Level | %wt of G | %wt of N | %wt of S |
| 1 | 24.11 | 24.73 | 23.76 |
| 2 | 24.19 | 24.11 | 24.58 |
| 3 | 24.4 | 24.29 | 24.54 |
| 4 | 24.05 | 23.62 | 23.86 |
| Delta | 0.35 | 1.11 | 0.82 |
| Rank | 3 | 1 | 2 |
Response table for S/N ratios compressive strength.
| Larger is better | |||
|---|---|---|---|
| Level | %wt of G | %wt of N | %wt of S |
| 1 | 25.17 | 24.01 | 24.84 |
| 2 | 24.77 | 25.65 | 24.91 |
| 3 | 24.56 | 25.42 | 24.7 |
| 4 | 24.76 | 24.17 | 24.81 |
| Delta | 0.6 | 1.65 | 0.2 |
| Rank | 2 | 1 | 3 |
Figure 6The main effect plots (a) tensile; (b) flexural; (c) compressive.
Figure 7Interaction plots (a) tensile; (b) flexural; (c) compressive.
Fiber composition (%wt) in four prior composites.
| Test Type | Experiments | Fiber composition (%wt) in a composite | Rank | ||||
|---|---|---|---|---|---|---|---|
| G | N | S | σmax | S/N | |||
| Tensile | 10 | 10 | 10 | 20 | 220.12 | 24.99031 | I |
| 12 | 10 | 20 | 10 | 216.26 | 24.82304 | II | |
| 2 | 5 | 10 | 10 | 207.22 | 24.44905 | III | |
| 15 | 5 | 15 | 10 | 195.44 | 23.99656 | IV | |
| Flexural | 9 | 10 | 5 | 15 | 210.43 | 24.89138 | I |
| 5 | 10 | 5 | 10 | 205.87 | 24.72271 | II | |
| 12 | 10 | 20 | 10 | 201.19 | 24.62279 | III | |
| 13 | 10 | 5 | 20 | 192.70 | 24.59479 | IV | |
| Compression | 2 | 5 | 10 | 10 | 308.55 | 26.02278 | I |
| 11 | 10 | 15 | 5 | 291.37 | 25.86181 | II | |
| 13 | 10 | 10 | 15 | 289.47 | 25.81876 | III | |
| 15 | 10 | 15 | 10 | 235.00 | 25.76138 | IV | |
Figure 8Stress-strain curves (a) tensile; (b) flexural; (c) compressive.
Figure 9Result comparison with [54].
Figure 10Normal probability plot (a) tensile; (b) flexural; (c) compressive.