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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).
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...
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...
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...
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...
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...
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...

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