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In this work, the shape optimization problem of a solid immersed in the incompressible fluid governed by Navier-Stokes equations is considered. Based on the continuous adjoint method, the shape gradie...
This is the second of three lectures prepared by the authors for the von Karman Institute that deal with the subject of aerodynamic shape optimization. In our first lecture we introduced some th...
Aeronautics, and in particular aerodynamics, has been one of the main technological drivers for the development of computational fluid dynamics (CFD).
In order to set the context for aerodynamic shape optimization, the airplane design process is summarized in the following paragraphs. It can generally be divided into three phases: conceptual design,...
During the last decade, aerodynamic shape optimization methods based on control theory have been intensively developed. The methods have proved to be very e ective for improving wing section shapes fo...
This paper compares the continuous and discrete viscous adjoint-based automatic aerodynamic optimization.
An adjoint-based Navier-Stokes design and optimization method for two-dimensional multi-element high-lift configurations is derived and presented. The compressible Reynolds-Averaged Navier-Stokes (RAN...
These Lecture Notes review the formulation and application of optimization techniques based on control theory for aerodynamic shape design in both inviscid and viscous compressible ow. The theory is a...
An aerodynamic shape optimization method that treats the design of complex aircraft configurations subject to high fidelity CFD, geometric constraints and multiple design points is described. The desi...
Select ADO-DG Case Studies in Aerodynamic Design Optimization
Aerodynamic Inverse Design and Shape Optimization via Control Theory     via Control Theory  Shape       font style='font-size:12px;'> 2015/6/18
Capability to predict the flow past an airplane in different flight regimes such as take off, cruise, flutter. 2 Interactive design calculations to allow immediate improvement 3 A...
Airplane Design with Aerodynamic Shape Optimization     Shape  Airplane Design       font style='font-size:12px;'> 2015/6/18
A light structure is needed to reduce W0. SFC is the province of the engine manufacturers. The aerodynamic designer should try to maximize VL D . This means the cruising speed V should be increase...
Airplane Design with Aerodynamic Shape Optimization     Airplane Design  aerodynamic       font style='font-size:12px;'> 2015/6/18
For a given stress σ, the required skin thickness varies inversely as the wing depth d. Thus weight can be reduced by increasing the thickness to chord ratio. But this will increase shock drag in th...
Mathematical Underpinnings of Aerodynamic Shape Optimization     aerodynamic  Mathematical Underpinnings       font style='font-size:12px;'> 2015/6/18
Regard the wing as a device to generate lift (with minimum drag) by controlling the flow. Apply theory of optimal control of systems governed by PDEs (Lions) with boundary control (the wing s...
The use of expensive simulations in engineering design optimization often rules out conventional techniques for design optimization for a variety of reasons, such as lack of smoothness, unavailabili...

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