2018
DOI: 10.1049/iet-nbt.2017.0320
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Comparative study on nanostructured order–disorder in the wing eyespots of the giant owl butterfly,Caligo memnon

Abstract: A characteristic feature of the giant owl butterfly, i.e. , is its big wing eyespot. This feature could serve as deceiving functionality for the butterfly against predators. As evidenced by scanning electron microscope (SEM) image on black part of eyespot, the scales on wing eyespot contain nanostructured ridges and cross-ribs. Applying direct measurement, statistical method, and Fourier analysis, the authors evidence that these nanostructures display order-disorder in their shape and position. The autocorrela… Show more

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Cited by 6 publications
(5 citation statements)
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“…These scales appear matte black, and are thus functionally tuned for anti‐reflectance. Other reports have studied the biophysics of light‐trapping by analogous scale structures, and converge in the finding that highly ordered structures are required for light manipulation . Our measurements of over 250 black scales recapitulate the finding that orderedness of scale ultrastructures, particularly crossrib width and spacing, is linked to light trapping in matte black scale types.…”
Section: Discussionsupporting
confidence: 83%
“…These scales appear matte black, and are thus functionally tuned for anti‐reflectance. Other reports have studied the biophysics of light‐trapping by analogous scale structures, and converge in the finding that highly ordered structures are required for light manipulation . Our measurements of over 250 black scales recapitulate the finding that orderedness of scale ultrastructures, particularly crossrib width and spacing, is linked to light trapping in matte black scale types.…”
Section: Discussionsupporting
confidence: 83%
“…From the Euler angles α ( t ), θ ( t ), and φ ( t ), flapping kinematic data can be obtained at any time. Fourier series combined with different coefficients can be used to describe any arbitrary curve [ 36 , 37 ], so the fitted curves of the three flapping angles can be described via the Fourier series. Figure 2 D shows the Euler angles of the hindwings during the beetle’s flapping flight.…”
Section: Resultsmentioning
confidence: 99%
“…The fitted curves can directly reflect the function of the wing‐flapping angles, which is also useful for inputting related functions in subsequent CFD analysis. Considering Fourier series combined with different coefficients can be used to describe an arbitrary curve [24]; here, the first four Fourier terms were chosen to describe the flapping‐wing motion of the hind wing accurately. The definition of position angle, elevation angle and rotation angle are given below: F )(t = n = 0 4 an cos nKt + bn sin nKt K = 2 πfc 2 U U = 2 θRf where n represents an integer changing from 0 to 4; t represents time; K represents the reduced frequency, which is 0.37; a n and b n represent the constant coefficients of the Fourier terms; f represents flapping‐wing frequency and is 68.7 Hz; c is the mean hind wing chord length, which is 11.677 mm; U is calculated to be 6.91 m/s, which represents the reference velocity at the wing tip; R is the length of the hind wing, which is measured to be 45.27 mm; θ is the wing beat amplitude and is about 70°.…”
Section: Resultsmentioning
confidence: 99%
“…The fitted curves can directly reflect the function of the wing-flapping angles, which is also useful for inputting related functions in subsequent CFD analysis. Considering Fourier series combined with different coefficients can be used to describe an arbitrary curve [24]; here, the first four Fourier terms were chosen to describe the flappingwing motion of the hind wing accurately. The definition of position angle, elevation angle and rotation angle are given below:…”
Section: Kinematic Modellingmentioning
confidence: 99%