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The results are compared with those from other research groups and those obtained using the fifth order WENO scheme and fourth order central differencing.
In this paper, we develop a three-dimensional parallel solver using the fifth order high-resolution weighted essentially non-oscillatory (WENO) finite difference scheme to perform extensive simulation for three-dimensional gaseous detonations.
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The equation of motion is solved numerically using the fourth order Runge Kutta method.
The reliability analysis was carried out using the First Order Reliability Method (FORM).
Autopilot control law has been designed for Micro Aerial Vehicle MAVV) using the second order sliding mode (SOSM) approach.
The final column of the table shows the calculated turbidity from our meter using the second order regression equation.
The problem is studied using the first order shear deformable (or the Mindlin) plate theory.
The DHSVM model was calibrated and validated using the second order watershed.
The equilibrium and stability equations are derived using the third order shear deformation plate theory.
The nonlinear system of equations is solved using the fourth order Runge Kutta method.
Finally, the governing equations are integrated using the fourth order Runge Kutta method.
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