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The Aerodynamic Measurement Technology and Ground Testing Conference will include papers related to all aspects of the science, technology, and application of aerodynamic measurements, from basic rese...
The Aerodynamic Measurement Technology and Ground Testing Conference will include papers related to all aspects of the science, technology, and application of aerodynamic measurements, from basic rese...
This conference presents the latest research in the development and application of aerodynamic deceleration systems and lifting parachutes, pararotators, sand inflatable decelerators for aerodynamic d...
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...
Every airplane has an associated external flow field that is extraordinarily rich in terms of its flow physics. It is intuitively obvious that the shape and configuration of th...
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 discusses the role that computational fluid dynamics plays in the design of aircraft. An overview of the design process is provided, covering some of the typical decisions that a desi...
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...
This paper describes the implementation of optimiza-tion techniques based on control theory for airfoil and wing design. The theory is applied to a system de- fined by the partial differential equatio...
Select ADO-DG Case Studies in Aerodynamic Design Optimization
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...

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