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Titlebook: Aerodynamics of a Lifting System in Extreme Ground Effect; Kirill V. Rozhdestvensky Book 2000 Springer-Verlag Berlin Heidelberg 2000 aerod

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期刊全稱Aerodynamics of a Lifting System in Extreme Ground Effect
影響因子2023Kirill V. Rozhdestvensky
視頻videohttp://file.papertrans.cn/151/150486/150486.mp4
發(fā)行地址There is no competitive book on the market.Includes supplementary material:
圖書封面Titlebook: Aerodynamics of a Lifting System in Extreme Ground Effect;  Kirill V. Rozhdestvensky Book 2000 Springer-Verlag Berlin Heidelberg 2000 aerod
影響因子This book is dedicated to the memory of a distinguished Russian engineer, Rostislav E. Alexeyev, who was the first in the world to develop the largest ground effect machine - Ekranoplan. One of Alexeyev‘s design concepts with the aerodynamic configuration of a jlying wing can be seen on the front page. The book presents a description of a mathematical model of flow past a lifting system, performing steady and unsteady motions in close proximity to the underlying solid surface (ground). This case is interesting for practical purposes because both the aerodynamic and the economic efficiency of the system near the ground are most pronounced. Use of the method of matched asymptotic expansions enables closed form solutions for the aerodynamic characteristics of the wings-in-ground effect. These can be used for design, identification, and processing of experimental data in the course of developing ground effect vehicles. The term extreme ground effect, widely used through- out the book, is associated with very small relative ground clearances of the order of 10% or less. The theory of a lifting surface, moving in immediate proximity to the ground, represents one of the few limiting cases
Pindex Book 2000
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https://doi.org/10.1007/978-3-8349-9933-7ct, the cruise speed of ground-effect vehicles can amount to half or more of the speed of sound. At the same time, it is known that the problem of unsteady subsonic flow is one of the most challenging in lifting surface theory; see Belotserkovsky et al. [139]. The complexity of the problem partly st
地板
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neue betriebswirtschaftliche forschung (nbf)e wing’s tips and are intended to decrease leakage of air from under the lifting system. Consequenly, the mounting of endplates results in the augmentation of lift or in a decrease of the induced drag for a given lift. In practice, the configuration of the endplates can vary. Figure 6.1 illustrates
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Trends in der Leadership-Forschung the craft from water. An efficient way to facilitate takeoff consists of blowing air under the main wing of the craft from special engines. This mode of vehicle operation is often called . or, briefly, .. Power augmentation provides additional dynamic head to support the vehicle at small speed and
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Trends in der Leadership-Forschungsentially, in the extreme ground effect, we study the limiting process, when the distance between two double (vortex) layers, representing the wing and its mirror image, becomes vanishingly small. In the limit, the two double layers merge into a . so that the procedure can be characterised as ... Th
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https://doi.org/10.1007/978-3-662-04240-3aerodynamics; aircraft construction; aircraft engineering; algorithm; lifting system; mathematical modeli
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