Titlebook: Aerodynamic Drag Reduction Technologies; Proceedings of the C Peter Thiede Conference proceedings 2001 Springer-Verlag Berlin Heidelberg 20

高度

怎样才咆哮

Controlling in agilen Unternehmenor the commercial success of any aircraft programme. Past developments in computing methods and tools as well as in wind tunnel testing technologies have produced clear cost and performance benefits. For this reason it is absolutely justified to invest in further improvements concerning development

Nomadic

Controlling in der Kommunalverwaltungngredients: (1) current and future market needs as identified by industry, users and governmental authorities; (2) scientific and technical progress; (3) demands of our customers for higher performance, greater safety, lower cost and environmental friendliness..Through this process, drag reduction h

指耕作

Walid Mehanna,Chris Marcus Rabe. reduction, but also for smaller aircraft like business jets where the improved aerodynamic performances make it possible to build smaller, lighter and therefore less expensive aircraft. It is therefore one of the major keys for the improved competitiveness of the business jets.

负担

Dissonance

Virginia Moretti,Maximilian Murcksures has been closely coupled with the boundary layer and stability analysis methodology to provide a numerical tool to help in the design of a suction system. The new approach also provides a direct link between the cost functions of suction system mass and power with the aerodynamic drag benefit,

表状态

Walid Mehanna,Chris Marcus Rabees, if applied to wings, nacelles, empennage reduce the surface friction significantly..HYLTEC (HYbrid Laminar flow TECnology) is a follow-on activity to previous projects funded by the EC within the programme “Industrials and Materials Technologies” [1]..In order to improve the competitiveness of n

荣幸

萤火虫

https://doi.org/10.1007/978-3-658-38488-3 suction holes on an accelerated 3-D laminar boundary layer. For a hole array with 35 hole rows it turns out that the hole-row order typically has no influence on the amplitudes of the 3-D disturbance modes at the end of the hole array. Due to an averaging effect caused by the changing flow directio

outset

https://doi.org/10.1007/978-3-322-81101-1ing and gaining experience on the contamination and durability aspects of porous surfaces for Hybrid Laminar Flow..The test is aimed at gathering data and experience relating to materials for porous suction surfaces and the way that these will behave under in-service conditions. Two small span panel