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We present results from the shape optimization of linked bodies for drag reduction in simulations of incompressible flow at moderate Reynolds numbers.
The main objective of this article is to investigate computational methods for the active control and drag optimization of incompressible viscous flow past cylinders, using the two-dimensional Navier Stokes equations as the flow model.
Several optimal design schemes for such components are given, and the effect of drag reduction of various optimization schemes is verified by experiments.The optimized elbows can effectively reduce local drag opposite VAC tubes by 9%10%%.
Multi-point aerodynamic shape design (implemented on a medium-size distributed memory cluster) deals with transonic wing optimization for minimum drag in the presence of multiple nonlinear constraints.
In the shape optimization of BWBUG, the lift to drag ratio is often used as the optimization target.
This paper describes a new technology of aerodynamic design based on CFD driven constrained optimization to minimum drag.
The robust airfoil optimization is aimed to minimize mean values and variances of drag coef-ficients while satisfying the lift and thickness constraints over a range of Mach numbers.
By the successive use of the global and local optimization methods, the drag of a multi-body aircraft configuration can be minimized for inviscid and viscous flow conditions while the baseline lift and wing weight are maintained.
Aim is the optimization of a cost functional based on drag and lift with respect to the position of the flaps as design parameters.
Additionally, the subsequent analysis and design optimization such as vibration of structure and disturbing frequencies needed an analytical and simple formation of drag history.
Correctly balancing the centrifugal force and the radial gas solid drag force requires an optimization of the fluidization chamber design for each given type of particles.
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