標(biāo)題: Titlebook: Control of Flow Instabilities and Unsteady Flows; G. E. A. Meier,G. H. Schnerr Book 1996 Springer-Verlag Wien 1996 flow.fluid mechanics.me [打印本頁(yè)] 作者: Hayes 時(shí)間: 2025-3-21 17:14
書目名稱Control of Flow Instabilities and Unsteady Flows影響因子(影響力)
書目名稱Control of Flow Instabilities and Unsteady Flows影響因子(影響力)學(xué)科排名
書目名稱Control of Flow Instabilities and Unsteady Flows網(wǎng)絡(luò)公開度
書目名稱Control of Flow Instabilities and Unsteady Flows網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Control of Flow Instabilities and Unsteady Flows被引頻次
書目名稱Control of Flow Instabilities and Unsteady Flows被引頻次學(xué)科排名
書目名稱Control of Flow Instabilities and Unsteady Flows年度引用
書目名稱Control of Flow Instabilities and Unsteady Flows年度引用學(xué)科排名
書目名稱Control of Flow Instabilities and Unsteady Flows讀者反饋
書目名稱Control of Flow Instabilities and Unsteady Flows讀者反饋學(xué)科排名
作者: Tortuous 時(shí)間: 2025-3-21 23:20
Book 1996plied control methods. Understanding and handling of control methods of nonlinear systems, typical of Fluid Mechanics, is the key to reduce losses and to improve the efficiency and safety of technical processes.作者: interference 時(shí)間: 2025-3-22 02:29 作者: A保存的 時(shí)間: 2025-3-22 05:49
https://doi.org/10.1007/978-3-7091-2688-2flow; fluid mechanics; mechanics; fluid- and aerodynamics作者: conjunctiva 時(shí)間: 2025-3-22 10:35 作者: ETHER 時(shí)間: 2025-3-22 15:20
Control of Flow Instabilities and Unsteady Flows978-3-7091-2688-2Series ISSN 0254-1971 Series E-ISSN 2309-3706 作者: ETHER 時(shí)間: 2025-3-22 17:03 作者: Rheumatologist 時(shí)間: 2025-3-23 00:26 作者: 植物群 時(shí)間: 2025-3-23 01:32 作者: expeditious 時(shí)間: 2025-3-23 08:06
Diskurstheorie als Forschungsperspektive reviewing what is known about the structure of a turbulent boundary layer, active and passive techniques offering nett drag benefits will be discussed. Emphasis will be put on the concepts which appear to have potential for possible transonic aircraft applications via manipulation of either the inn作者: 親屬 時(shí)間: 2025-3-23 11:20
https://doi.org/10.1007/978-3-658-40282-2n stability or excitation of boundary layers and on separation in flows. These additional influences are active influences because they imply an unsteady or at least adaptive change of boundary or flow conditions with the help of external energy..Examples given in the lectures are the influence of p作者: jovial 時(shí)間: 2025-3-23 14:32 作者: 整頓 時(shí)間: 2025-3-23 20:33 作者: Anemia 時(shí)間: 2025-3-23 23:11 作者: brother 時(shí)間: 2025-3-24 03:11
Optimal Control and Other Complex Systems Paradigms in the Context of Turbulent Flows,ple, e.g. a fixed point dynamics, it is necessary to perturb it in order to reconstruct the model. Of course, perturbations are also necessary to control a system. The problem with these perturbations is that they may activate additional variables which are not included in the simple model. Thus, th作者: Jejune 時(shí)間: 2025-3-24 07:17 作者: 壓迫 時(shí)間: 2025-3-24 12:05
Passive Ventilation of Shocks in Steady and Unsteady Internal Flows,y supersonic compressor flow. Alternatively we show the effectiveness of ventilation by very thin slits instead of a cavity covered by a porous blade..Finally we apply the method of ventilation to unsteady internal transonic flow. Experiments and numerical results of the Euler equations for inviscid作者: 無(wú)意 時(shí)間: 2025-3-24 15:57
Instabilities of Compressible Flows with Internal Heat Addition,choking (Delale, Schnerr and Zierep [1]) with steady or unsteady moving shock waves and instabilities like high frequency pressure oscillations. Self-excitation develops because of the instantaneous interaction of the shock with the phase transition process. Control and handling of these steady and 作者: 砍伐 時(shí)間: 2025-3-24 21:47
https://doi.org/10.1007/978-3-658-40274-7ple, e.g. a fixed point dynamics, it is necessary to perturb it in order to reconstruct the model. Of course, perturbations are also necessary to control a system. The problem with these perturbations is that they may activate additional variables which are not included in the simple model. Thus, th作者: 退潮 時(shí)間: 2025-3-25 00:35
https://doi.org/10.1007/978-3-658-40282-2igh angles of incidence can be influenced. For this purpose normal sound waves from a loudspeaker can be used. Another more efficient technique uses sound waves focused by a mirror on a small region of a certain wing area. This results in a stronger localised excitation which reduces laminar flow se作者: Perceive 時(shí)間: 2025-3-25 03:46
Diskurstheorie als Forschungsperspektivey supersonic compressor flow. Alternatively we show the effectiveness of ventilation by very thin slits instead of a cavity covered by a porous blade..Finally we apply the method of ventilation to unsteady internal transonic flow. Experiments and numerical results of the Euler equations for inviscid作者: 間接 時(shí)間: 2025-3-25 08:10 作者: 躺下殘殺 時(shí)間: 2025-3-25 11:43
Control of Laminar-Turbulent Transition for Skin Friction Drag Reduction,and illustrated by experimental results obtained in wind tunnel or in free flight conditions. Wave cancellation techniques are also presented. An important part of the paper is devoted to the use of the linear stability theory as a practical tool for transition prediction.作者: 動(dòng)物 時(shí)間: 2025-3-25 17:03
Diskurstheorie als Forschungsperspektive the abilities of applied methods. Finally, the material presented here, describes some of the modifications being introduced to standard passive control in order to improve the effectiveness of ventilation.作者: 顯微鏡 時(shí)間: 2025-3-25 22:27
Passive Control of Shock/Boundary Layer Interaction, the abilities of applied methods. Finally, the material presented here, describes some of the modifications being introduced to standard passive control in order to improve the effectiveness of ventilation.作者: Reservation 時(shí)間: 2025-3-26 00:28 作者: myalgia 時(shí)間: 2025-3-26 06:27 作者: NUL 時(shí)間: 2025-3-26 11:20
Diskurstheorie als Forschungsperspektive experimental and numerical results concerning the following techniques: wall suction, injection, active and selective control of turbulent boundary layers, passive control of turbulent boundary layers using LEBUs and Riblets. Some turbulent separation flow control will be briefly evoked.作者: 說(shuō)明 時(shí)間: 2025-3-26 13:32
Developments in Stability Theory,isk, and the stability of a range of wake flows. All these situations apply very much to parallel flows, however, and in order to handle non-parallel flows one must find ways of connecting the local, quasi-parallel properties of the flow to the global dynamics.作者: 有毛就脫毛 時(shí)間: 2025-3-26 18:13
Control of Turbulent Flows for Skin Friction Drag Reduction, experimental and numerical results concerning the following techniques: wall suction, injection, active and selective control of turbulent boundary layers, passive control of turbulent boundary layers using LEBUs and Riblets. Some turbulent separation flow control will be briefly evoked.作者: temperate 時(shí)間: 2025-3-26 22:18
0254-1971 ory and applied control methods. Understanding and handling of control methods of nonlinear systems, typical of Fluid Mechanics, is the key to reduce losses and to improve the efficiency and safety of technical processes.978-3-211-82807-6978-3-7091-2688-2Series ISSN 0254-1971 Series E-ISSN 2309-3706作者: 潰爛 時(shí)間: 2025-3-27 03:12
https://doi.org/10.1007/978-3-658-40274-7and illustrated by experimental results obtained in wind tunnel or in free flight conditions. Wave cancellation techniques are also presented. An important part of the paper is devoted to the use of the linear stability theory as a practical tool for transition prediction.作者: Promotion 時(shí)間: 2025-3-27 08:08 作者: 偶然 時(shí)間: 2025-3-27 10:49
Optimal Control and Other Complex Systems Paradigms in the Context of Turbulent Flows,mplex systems. In these lectures, we present new principles and methodologies of complex systems research, that may help to understand and control the dynamics of turbulent flows. The dynamics of a high dimensional complex system can in many cases be estimated from simple models such as coupled maps作者: fatty-streak 時(shí)間: 2025-3-27 16:42
Control of Laminar-Turbulent Transition for Skin Friction Drag Reduction,tricted to low speed and transonic problems. The stabilizing or destabilizing effects of pressure gradient, heating/cooling and suction are explained and illustrated by experimental results obtained in wind tunnel or in free flight conditions. Wave cancellation techniques are also presented. An impo作者: opinionated 時(shí)間: 2025-3-27 19:53 作者: 慎重 時(shí)間: 2025-3-28 00:40
Active Control of Boundary Layer and Separation,n stability or excitation of boundary layers and on separation in flows. These additional influences are active influences because they imply an unsteady or at least adaptive change of boundary or flow conditions with the help of external energy..Examples given in the lectures are the influence of p作者: 協(xié)迫 時(shí)間: 2025-3-28 06:06
Passive Control of Shock/Boundary Layer Interaction,g material about the interaction field structure and its behaviour under the influence of key parameters. Besides, various theoretical approaches are presented and explained, the historical as well as the modern ones. A comparison of the theoretical results with corresponding experiments illustrates作者: graphy 時(shí)間: 2025-3-28 07:11
Passive Ventilation of Shocks in Steady and Unsteady Internal Flows,rom blade vibrations or aerodynamic disturbances at the in- or outflow boundaries may cause structural failure of the blading and, possibly, extensive damage of the engine. In the transonic flow regime waves propagate in the flow field and displace shock waves, therefore the time dependent shock mov作者: motor-unit 時(shí)間: 2025-3-28 13:08
Instabilities of Compressible Flows with Internal Heat Addition,lets prevail in many engineering problems in fluid mechanics and industry. Phase transition of rapidly expanding vapor or vapor/carrier gas mixtures is usually not observed at thermodynamic equilibrium. Because heat is added to the flow by condensation of a component of the fluid itself, flow and he作者: 宏偉 時(shí)間: 2025-3-28 18:07 作者: 生氣的邊緣 時(shí)間: 2025-3-28 21:15
