標(biāo)題: Titlebook: New Results in Numerical and Experimental Fluid Mechanics VI; Contributions to the Cameron Tropea,Suad Jakirlic,Heinz H?nlinger Conference [打印本頁(yè)] 作者: 貧血 時(shí)間: 2025-3-21 16:25
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI影響因子(影響力)
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI影響因子(影響力)學(xué)科排名
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI網(wǎng)絡(luò)公開(kāi)度
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI被引頻次
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI被引頻次學(xué)科排名
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI年度引用
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI年度引用學(xué)科排名
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI讀者反饋
書(shū)目名稱New Results in Numerical and Experimental Fluid Mechanics VI讀者反饋學(xué)科排名
作者: 溫和女人 時(shí)間: 2025-3-21 22:04 作者: 攝取 時(shí)間: 2025-3-22 03:08
Multiple Discipline Take-Off Weight Minimization for a Supersonic Transport Aircraftst flight time is spent-the disciplines aerodynamics and structures are modelled at high fidelity while other contributing disciplines and flight phases are modelled less accurate. For a generic long-range mission the impact of the supersonic cruise-speed on the minimal take-off weight (enabling to cruise this long range mission) is addressed.作者: 狗舍 時(shí)間: 2025-3-22 06:01
High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Propertieshe boundary layer properties. Three airfoils were created for transonic free flight conditions with very similar aerodynamic performance, but different boundary layer developments on the upper surface. The performance and boundary layer properties of the airfoils were discussed and validated by RANS computations.作者: Assemble 時(shí)間: 2025-3-22 11:00 作者: 出生 時(shí)間: 2025-3-22 14:16
Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow plane was investigated. Flexibility of the wing-body model was considered and the influence of aeroelasticity on the SCB performance was examined. RANS simulations with the DLR FLOWer code showed, that both the influence of trimming as well as of aeroelasticity is negligible for SCB design.作者: 騷擾 時(shí)間: 2025-3-22 20:09 作者: 驚呼 時(shí)間: 2025-3-23 00:52
Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted oresolution was used to investigate the heat flux fluctuation on the surface of a slightly heated cylinder. Comparative investigations showed qualitative correlations between the pressure and heat flux fluctuations around the cylinder and on its free-end. Several flow features could be identified by means of time-resolved surface measurements.作者: 褻瀆 時(shí)間: 2025-3-23 02:30 作者: 議程 時(shí)間: 2025-3-23 08:03
Three-Dimensional Discontinuous Galerkin Codes to Simulate Viscous Flow by Spatial Discretization ofn extension will be provided to include both three-dimensional flows and curved elements to properly represent three-dimensional bodies with curvature. Some results, like Sows around a sphere and around an Onera M6 wing, are calculated and compared with experiments.作者: 下級(jí) 時(shí)間: 2025-3-23 12:37
1612-2909 . Symposium of the STAB (German Aero-space Aerodynamics Association). In this association all those German scientists and engineers from universities, research establishments and industry are involved, who are doing research and project work in numerical and experimental fluid mechanics and aerodyna作者: 胖人手藝好 時(shí)間: 2025-3-23 14:09
URANS and DES Simulation of Flow Around a Rectangular Cylindering the basic unsteady flow phenomena in the considered cases. These results are further confirmed by the DES method, which provides information about the instantaneous flow variables and offers a deeper insight into the flow physics.作者: 不可比擬 時(shí)間: 2025-3-23 18:14
Numerical Simulation of a Wing with a Gapless High-Lift System Using Circulation Controlystems. The promising results of the 2D simulations motivate applications to a wing-body configuration. The results show that a gapless high-lift system equipped with circulation control has the ability to provide sufficient lift for take off, climb and landing.作者: 是剝皮 時(shí)間: 2025-3-24 01:17 作者: Observe 時(shí)間: 2025-3-24 03:09
Design of a Retrofit Winglet for a Transport Aircraft with Assessment of Cruise and Ultimate Structu evaluate ultimate structural loading. Comparing the results of the rigid wing with the deformed wing the wing root bending moment and the bending moment of the device is clearly reduced for the deformed wing. Thereby the advantage to which an implementation of the described method for future design processes would lead becomes apparent.作者: 性冷淡 時(shí)間: 2025-3-24 07:25 作者: 委托 時(shí)間: 2025-3-24 10:55 作者: NATAL 時(shí)間: 2025-3-24 16:54
An Airbrake Design Methodology for Steep Approachesng mounted over the wing region, dorsal airbrakes utilise the accelerated flow field around the airframe and generate a high amount of drag. Neither the lift nor the pitch-moment are influenced considerably through deployment of the dorsal airbrakes. This paper presents a methodology and principles 作者: 宴會(huì) 時(shí)間: 2025-3-24 20:25
Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Modeld Reynoldsaveraged Navier Stokes Code TAU, are in good agreement with the experiments. They show a separation of the boundary layer starting at the trailing edge with high crossflow velocities at the outer tailplane. Depending on the boundary-layer transition, the stall occurs abruptly for natural t作者: 可卡 時(shí)間: 2025-3-25 00:59 作者: 預(yù)防注射 時(shí)間: 2025-3-25 05:50 作者: Anal-Canal 時(shí)間: 2025-3-25 09:35 作者: Confidential 時(shí)間: 2025-3-25 13:50 作者: 拍翅 時(shí)間: 2025-3-25 18:50 作者: 緩解 時(shí)間: 2025-3-25 22:39
K. Richter,S. Koch,H. Rosemannom the data of two leading crowdfunding platforms, we analyzed the strategic importance of highlighting a single or multiple trendy topics on the funding outcomes—both the amount of funding pledged and the additional dollars pledged to a project. Our results suggest that crowdfunding projects featur作者: Irremediable 時(shí)間: 2025-3-26 02:09 作者: Digitalis 時(shí)間: 2025-3-26 07:31
Arne Grote,Rolf Radespielountries regarding their development factors. The main data consist of two indicators from Global Entrepreneurship Monitor (GEM)—physical infrastructure and internal market dynamics—and four indices from Global Innovation Index (GII)—infrastructure, market sophistication, business sophistication, an作者: MERIT 時(shí)間: 2025-3-26 09:34 作者: obviate 時(shí)間: 2025-3-26 16:21 作者: 制造 時(shí)間: 2025-3-26 20:00
Axel Raichle,Stefan Melber-Wilkending,Jan Himischted and co- ? to specify current SEA-related methodologies and ordinated several international expert meetings in procedures, to identify major deficiencies and to the field of "Environmental Impact Assessment". propose means of overcoming these, The participants of these meetings were drawn from ? 作者: 和平主義者 時(shí)間: 2025-3-26 21:42 作者: 拋棄的貨物 時(shí)間: 2025-3-27 01:49
Benedikt K?nig,Martin P?tzold,Thorsten Lutz,Ewald Kr?merand satisfactory, feasibility in trying to express landscape values by using the language of numbers. This chapter, after a mandatory general introduction about the indicator concept, examines the problems related to the use of landscape indicators and presents some of the most interesting arrays of作者: 下級(jí) 時(shí)間: 2025-3-27 08:58 作者: 現(xiàn)暈光 時(shí)間: 2025-3-27 10:57 作者: MUT 時(shí)間: 2025-3-27 17:14
D. Pallek,F. Klingee different categories of territorial variables—environmental, social, landscape, and economical-institutional—could describe the current characteristics of a landscape with future scenarios proposed by the plan. The typology of data we can obtain from this assessment technique is expressed by a num作者: Outwit 時(shí)間: 2025-3-27 18:33 作者: Distribution 時(shí)間: 2025-3-28 01:18 作者: carotid-bruit 時(shí)間: 2025-3-28 02:30 作者: 走路左晃右晃 時(shí)間: 2025-3-28 06:33 作者: 做事過(guò)頭 時(shí)間: 2025-3-28 13:12 作者: Microgram 時(shí)間: 2025-3-28 16:10
B. Anil Mertolvancements are drastically shaping different industries, including entrepreneurs and their businesses, as well as the investors of entrepreneurial firms. Consequently, a growing number of entrepreneurs have incorporated these technological advancements (henceforth called advanced technologies) in th作者: SHOCK 時(shí)間: 2025-3-28 20:51
K. Richter,S. Koch,H. Rosemannvancements are drastically shaping different industries, including entrepreneurs and their businesses, as well as the investors of entrepreneurial firms. Consequently, a growing number of entrepreneurs have incorporated these technological advancements (henceforth called advanced technologies) in th作者: 高度 時(shí)間: 2025-3-28 22:58 作者: 合唱團(tuán) 時(shí)間: 2025-3-29 05:37
Arne Grote,Rolf Radespiel The strategic management philosophy can be applied to the nexus of entrepreneurship, innovation, and economy to foster development and competitiveness in the entrepreneurial sector. Also, the pivotal elements of the strategic management model can be replicated with the critical components of entrep作者: Gyrate 時(shí)間: 2025-3-29 09:18
Claudio Mannini,Ante Soda,Ralph Vo?,Günter Scheweth reference both to the development of the notion over the time and the way it relates to other fields of study, like Social and Humane Entrepreneurship. For the purpose of this investigation, . and . were used as databases. 183 articles (93 full papers and 90 abstracts) were finally selected and e作者: gnarled 時(shí)間: 2025-3-29 14:15
Ralf H?rnschemeyer,Christoph Rixen,Sebastian Kauertz,Günther Neuwerth,Rolf Henkeon is the effect we take into account. Indeed, the paper aims at investigating how SEA is effective in evaluating it and, in case, in reducing the land consumption generated by the urban plans at municipal scale. The analysis considers the Italian context, in particular the Lombardy Region, which wa作者: TERRA 時(shí)間: 2025-3-29 16:26 作者: Dappled 時(shí)間: 2025-3-29 20:42 作者: Spangle 時(shí)間: 2025-3-30 02:48
K.-C. Pfingsten,R. Radespielt in urban planning practices, it relies on the support of a qualified study centre: the Landscape Observatory. This centre was created to respond to the need to study the landscape, prepare proposals and sensitise Catalan society to the need for better protection, management and planning of the lan作者: CHIP 時(shí)間: 2025-3-30 08:00 作者: 蝕刻 時(shí)間: 2025-3-30 10:41
Jens Ortmanns,Christian J. K?hler,Rolf Radespiel designed to evaluate the effects of human actions on them. The environmental evaluation methods, born in the USA, have known different disciplinary evolutions according to the following factors: firstly, regarding the object to assess; secondly, pertaining to the national juridical framework; and t作者: 增長(zhǎng) 時(shí)間: 2025-3-30 13:58 作者: invade 時(shí)間: 2025-3-30 17:14
D. Pallek,F. Klingehe landscape. In fact, while the evaluation of components such as water, soil, and atmosphere has already been consolidated using environmental indicators, analysing landscape components—in addition to “cultural” components—is more arduous. There are three essential elements functional to landscape 作者: MIRTH 時(shí)間: 2025-3-30 23:28
Matthew Robinson,Jan Martinez Schramm,Klaus Hannemanntions), and self-enforcing dynamic processes. Paradigms that aim to maintain structure in the relations between actors become subjects for modifications or replacement as dynamic processes unfold, leading to tensions when negotiating decisions. As this research project argues, managing bargaining du作者: VEIL 時(shí)間: 2025-3-31 04:25
U. Herrmanntions), and self-enforcing dynamic processes. Paradigms that aim to maintain structure in the relations between actors become subjects for modifications or replacement as dynamic processes unfold, leading to tensions when negotiating decisions. As this research project argues, managing bargaining du作者: muscle-fibers 時(shí)間: 2025-3-31 07:15 作者: 避開(kāi) 時(shí)間: 2025-3-31 10:28
Frieder L?rcher,Gregor Gassner,Claus-Dieter Münztions), and self-enforcing dynamic processes. Paradigms that aim to maintain structure in the relations between actors become subjects for modifications or replacement as dynamic processes unfold, leading to tensions when negotiating decisions. As this research project argues, managing bargaining du作者: intimate 時(shí)間: 2025-3-31 15:56
An Airbrake Design Methodology for Steep Approachesft (A/C) mainly depends on its high-lift system, while additional means can also help to increase this capability by generating drag. However, a desirable drag generation method should not degrade the high lift performance of the A/C. Otherwise, in order to achieve the same amount of lift force as b作者: 腐爛 時(shí)間: 2025-3-31 20:00
High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Propertiesnsport aircraft wing. In contrast to conventional low Reynolds number design methods, this method exploits full aerodynamic performance and controls the boundary layer properties. Three airfoils were created for transonic free flight conditions with very similar aerodynamic performance, but differen作者: 愛(ài)得痛了 時(shí)間: 2025-3-31 21:56
Numerical Analysis of Wing Vorticeswth of shortwave co-operative elliptical and long-wave Crow instabilities leads to a pronounced decay of its vorticity distribution. The four-vortex system possesses a smaller decay rate than the two-vortex system.作者: 向下五度才偏 時(shí)間: 2025-4-1 03:04
Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model configuration is numerically optimised to obtain large Reynolds numbers at the horizontal tailplane in a wind tunnel of limited size. It consists of a fuselage, a detachable horizontal tailplane and a tip-truncated wing, that mounts the model to the turntables of the closed test section. The wing w作者: mastoid-bone 時(shí)間: 2025-4-1 08:45 作者: COLON 時(shí)間: 2025-4-1 10:21 作者: 絕食 時(shí)間: 2025-4-1 15:51
A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Enginees a discontinous pressure jump to the flow. The topology of the grid maintains fluxes conservative through the disk. The load of the disk is calculated by time averaging the sectional load of a rotating blade. The sectional load is calculated with the blade element theory for a propeller of a sailp
