Sentence examples for length of wing from inspiring English sources
For example, in some insects one can measure body length, wing length, wing width, number and length of wing veins, or another trait.
At wind tunnel test, the chord length of wing model was set at 160 mm and the wingspan was set at 226 mm in order to fit for wind tunnel measurement section size and set the Re number as 105.
Here, we only used mean length of wing and outermost and central tail feathers measured with a ruler to the nearest mm, keel length and beak length, width and height, and tarsus length with a digital caliper to the nearest 0.01 mm and body mass to the nearest 0.1 g with a Pesola spring balance.
All individuals were weighed (in g) and standard body measurements were taken (in mm): length of wing chord, bill, culmen, seventh primary, tail and tarsus.
Closed form expressions for the instantaneous anisotropic compliance tensor with respect to the key physical parameters of the wing-cracks (the number density of cracks, the pre-existing flaw orientations and flaw sizes, the instantaneous length of wing-cracks, and the friction coefficient on the flaw surfaces) are derived through a kinematic approach.
The analytical parameters are width, thickness of steel tube, length, thickness of wing plate, strength of steel, and eccentricity of rebar.
According to the length of the wing, adults BPH are biomorphic with varying wing lengths.
The moment of inertia for the wing is then: I = \frac{m\ell^3}{3} Where l is the length of the wing (1 cm) and m is the mass of two wings, which may be typically 10−3 g.
This indicated that the fly was switching muscles on the side of the flipped wing into a lower "gear," shortening the length of that wing's beats (as shown by the green portions of the graph in the video) to allow the fly to turn, the team reports online today in the Journal of the Royal Society Interface.
To solve the dynamic equations for the wing where the extracellular matrix was distally ablated (ECM_DistCut) and for dumpyov1 mutant wings, a new dynamical equation for the length of the wing L is added, Equation 74 (94) γ d L d t = − h σ x x − k P D (L − x HB ).
Because the vertical tail fin was only slightly shorter than the length of each wing and nearly as aerodynamically effective, it could act as a wing on rudder application (a phenomenon known as "Dutch roll").
