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The steady cooling load is obtained by using a fin equation.
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The aim of the present study is to classify the Noether point symmetries of a fin equation.
In this study we analyze the Noether symmetry group classification of a nonlinear fin equation, which is a second-order nonlinear ordinary differential equation.
DNA was isolated from fin clips using a new method developed by us [ 52].
Briefly, DNA was extracted from adipose fin tissue and from fry caudal fin tissue using a salt-based method (Aljanabi and Martinez 1997).
Genomic DNA was isolated from pectoral fin clips using a DNeasy Tissue Kit (Qiagen).
DNA was extracted from fin clips using a standard phenol/chloroform protocol.
Genomic DNA was extracted from fin clips using a modified version of Aljanabi and Martinez [ 63].
DNA was extracted from adipose fin and pelvic fin clip (2 mm) using a modified version of Aljanabi and Martinez (1997) salt extraction method.
You can use an equation to calculate this.
The coupling between the wing (fin) motion and the induced aerodynamics using a doublet-lattice unsteady aerodynamics code is described.
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