標題: Titlebook: Aerodynamics of a Lifting System in Extreme Ground Effect; Kirill V. Rozhdestvensky Book 2000 Springer-Verlag Berlin Heidelberg 2000 aerod [打印本頁] 作者: cerebral 時間: 2025-3-21 16:45
書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect影響因子(影響力)
書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect影響因子(影響力)學科排名
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書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect被引頻次
書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect被引頻次學科排名
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書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect年度引用學科排名
書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect讀者反饋
書目名稱Aerodynamics of a Lifting System in Extreme Ground Effect讀者反饋學科排名
作者: saphenous-vein 時間: 2025-3-21 22:26 作者: SEVER 時間: 2025-3-22 00:43
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作者: 圓木可阻礙 時間: 2025-3-22 05:32
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 作者: fidelity 時間: 2025-3-22 12:13 作者: reflection 時間: 2025-3-22 14:12
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 作者: MAG 時間: 2025-3-22 17:27
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作者: CREEK 時間: 2025-3-22 22:38 作者: 天然熱噴泉 時間: 2025-3-23 04:43
https://doi.org/10.1007/978-3-662-04240-3aerodynamics; aircraft construction; aircraft engineering; algorithm; lifting system; mathematical modeli作者: Accord 時間: 2025-3-23 08:51 作者: 敲詐 時間: 2025-3-23 10:51 作者: genesis 時間: 2025-3-23 16:29 作者: Omnipotent 時間: 2025-3-23 19:49
Nonlinear Flow Problems for a Lifting System in the Extreme Ground Effect,. Essentially, as discussed at length in section 2, the procedure for the solution uses the assumption that, for . ? 1 and ε = O(.), nonlinear effects exhibit themselves mainly in the narrow channel under the foil. The foil and the corresponding coordinate system are shown in Fig. 4.1.作者: brassy 時間: 2025-3-24 01:12
The Influence of Endplates, Flaps, and Slots,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 schematically some of the possibilities.作者: Arctic 時間: 2025-3-24 06:14
Kirill V. RozhdestvenskyThere is no competitive book on the market.Includes supplementary material: 作者: BINGE 時間: 2025-3-24 08:30
http://image.papertrans.cn/a/image/150486.jpg作者: 共同時代 時間: 2025-3-24 10:58 作者: HUMP 時間: 2025-3-24 15:01
https://doi.org/10.1007/978-3-8349-9933-7To reduce a nonlinear formulation to the linear theory, one has to assume that the deflections of the surfaces of the wing, its vortex wake, and the ground, respectively, from horizontal planes . = .. and . = 0 are small compared to the ground clearance ., i.e., 作者: Cpap155 時間: 2025-3-24 20:41 作者: HALO 時間: 2025-3-24 23:42
Introduction,This book discusses the aerodynamics of vehicles, that utilize the favorable effect of the proximity to an underlying surface upon their performance. Although this underlying surface may be not only land, but also water, snow, or ice, it will be called ..作者: 生銹 時間: 2025-3-25 06:41
The Linear Theory of a Lifting System Moving Close to the Ground,To reduce a nonlinear formulation to the linear theory, one has to assume that the deflections of the surfaces of the wing, its vortex wake, and the ground, respectively, from horizontal planes . = .. and . = 0 are small compared to the ground clearance ., i.e., 作者: 不妥協(xié) 時間: 2025-3-25 10:59
The Aerodynamic Efficiency of a Wing in the Extreme Ground Effect,The theory of a wing in the extreme ground effect, as developed herein, enables us to formulate a number of extremal problems, which are of both theoretical and practical interest.作者: Accommodation 時間: 2025-3-25 13:07 作者: padding 時間: 2025-3-25 17:22
https://doi.org/10.1007/978-3-8349-9933-7teady subsonic flow is one of the most challenging in lifting surface theory; see Belotserkovsky et al. [139]. The complexity of the problem partly stems from the fact that in a compressible fluid the perturbations propagate with finite speeds.作者: 尊敬 時間: 2025-3-25 21:23 作者: 形容詞詞尾 時間: 2025-3-26 01:24 作者: FUSC 時間: 2025-3-26 06:02
neue betriebswirtschaftliche forschung (nbf)tions, because the influence of waves upon the aerodynamics of such a vehicle is in fact predominantly due to the corresponding variation of the geometry of the gap between the wing and the sea surface.作者: infatuation 時間: 2025-3-26 08:38 作者: 熱心 時間: 2025-3-26 16:29
Book 2000 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 t作者: 排名真古怪 時間: 2025-3-26 19:29 作者: Watemelon 時間: 2025-3-26 23:19 作者: 抒情短詩 時間: 2025-3-27 01:50 作者: Visual-Acuity 時間: 2025-3-27 06:03
Trends in der Leadership-Forschungting spray effects, and the transient motion of the vehicle. In what follows, only very simplified models of power-augmented flows will be considered for a lifting system moving very close to the underlying surface.作者: 有權 時間: 2025-3-27 12:18
Schematized Flow Models for a Power-Augmented Lifting System,ting spray effects, and the transient motion of the vehicle. In what follows, only very simplified models of power-augmented flows will be considered for a lifting system moving very close to the underlying surface.作者: Wordlist 時間: 2025-3-27 13:47 作者: Endometrium 時間: 2025-3-27 18:40
Equations and the Stability of Motion of a Lifting System in the Extreme Ground Effect,作者: CHIP 時間: 2025-3-28 01:20 作者: 常到 時間: 2025-3-28 02:45 作者: 挑剔為人 時間: 2025-3-28 06:48
ely 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 cases978-3-642-08556-7978-3-662-04240-3作者: 尾隨 時間: 2025-3-28 12:38
Integral Formulations for Lifting Surfaces in the Extreme Ground Effect,pproach in the aerodynamics of wings in the ground effect was first introduced by Panchenkov [64]. In what follows, all derivations will be based on a different scheme of quadruplication proposed in [66].作者: 樂章 時間: 2025-3-28 15:56 作者: Albinism 時間: 2025-3-28 20:10 作者: 迷住 時間: 2025-3-29 02:32
Nonlinear Flow Problems for a Lifting System in the Extreme Ground Effect,. Essentially, as discussed at length in section 2, the procedure for the solution uses the assumption that, for . ? 1 and ε = O(.), nonlinear effects exhibit themselves mainly in the narrow channel under the foil. The foil and the corresponding coordinate system are shown in Fig. 4.1.作者: Expand 時間: 2025-3-29 05:10 作者: infarct 時間: 2025-3-29 10:00
The Influence of Endplates, Flaps, and Slots,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 作者: BACLE 時間: 2025-3-29 15:05
The Aerodynamics of a Lifting System Near Curved Ground,rough seas. The approach of matched asymptotic expansions furnishes a simplified mathematical model of the unsteady aerodynamics of the wing-in-groundeffect vehicle, based on the idea of domination of the channel flow in the extreme ground effect. This concept seems to be promising for wave perturba作者: VAN 時間: 2025-3-29 16:36
Schematized Flow Models for a Power-Augmented Lifting System, 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 作者: cumber 時間: 2025-3-29 22:56
Integral Formulations for Lifting Surfaces in the Extreme Ground Effect,sentially, 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作者: regale 時間: 2025-3-30 01:55 作者: AUGUR 時間: 2025-3-30 07:51
