標(biāo)題: Titlebook: New Results in Numerical and Experimental Fluid Mechanics VII; Contributions to the Andreas Dillmann,Gerd Heller,Wolfgang Schr?der Conferen [打印本頁] 作者: Tamoxifen 時間: 2025-3-21 19:42
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII影響因子(影響力)
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII影響因子(影響力)學(xué)科排名
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII網(wǎng)絡(luò)公開度
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII被引頻次
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII被引頻次學(xué)科排名
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII年度引用
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII年度引用學(xué)科排名
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII讀者反饋
書目名稱New Results in Numerical and Experimental Fluid Mechanics VII讀者反饋學(xué)科排名
作者: 猛擊 時間: 2025-3-21 22:25 作者: 羊欄 時間: 2025-3-22 01:34
Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experimentde-wall. Results show that the effect of the sidewalls is similar to an offset in the angle of attack (but can only partially be corrected by a change in .), and that this effect is proportional to the lift and Mach number. These results were used in the design phase for the iGREEN wing-tailplane interference experiment.作者: 陰謀小團(tuán)體 時間: 2025-3-22 05:55
Application of the Immersed Boundary Method for the Simulation of Incompressible Flows in Complex anf this approach for flow simulations in complex and moving geometries are characterised. Simple validation test cases are addressed first, followed by a moving boundary example and more complex geometries like the Weibel lung model.作者: 即席演說 時間: 2025-3-22 09:09 作者: 急性 時間: 2025-3-22 15:58
New Results in Numerical and Experimental Fluid Mechanics VII978-3-642-14243-7Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: 狗窩 時間: 2025-3-22 18:44 作者: hypnotic 時間: 2025-3-23 00:20
tors, frustrated with tedious and time-consuming decision-making—for example during single negotiation rounds—seek both general and mini-agreements, including framework agreements, and implement plans that intend to provide structures to the social relations and frameworks of future decisions. Never作者: 蕨類 時間: 2025-3-23 01:35 作者: 偽書 時間: 2025-3-23 07:12
Giuseppe Bonfigli,Patrick Jennytors, frustrated with tedious and time-consuming decision-making—for example during single negotiation rounds—seek both general and mini-agreements, including framework agreements, and implement plans that intend to provide structures to the social relations and frameworks of future decisions. Never作者: 整體 時間: 2025-3-23 09:54
Z. -H. Han,S. G?rtz,R. Hainich in turn potentially makes the entire enterprise more virtuous and effective via, for example, improved climate. In other words, virtuousness has spirals that yield relational network outcomes. Followers’ virtuousness may also be useful in contexts where leadership is ineffectual. Virtuousness in作者: 粘 時間: 2025-3-23 15:50 作者: 擺動 時間: 2025-3-23 18:58
Emre ?zkaya,Nicolas R. Gaugerich in turn potentially makes the entire enterprise more virtuous and effective via, for example, improved climate. In other words, virtuousness has spirals that yield relational network outcomes. Followers’ virtuousness may also be useful in contexts where leadership is ineffectual. Virtuousness in作者: Slit-Lamp 時間: 2025-3-24 01:22
Bernhard Eisfeld,Tobias Knopp,Javier Bartolome Calvoprove. The condition, worldview, orientation, expectations, and responses (see figure 3.1) for this state are different from those of normalcy or positive deviance. Followers in this state seek to change the negative or bad influence situation to something better. Recall that value in this state is 作者: 使更活躍 時間: 2025-3-24 03:45
Tobias Knoppprove. The condition, worldview, orientation, expectations, and responses (see figure 3.1) for this state are different from those of normalcy or positive deviance. Followers in this state seek to change the negative or bad influence situation to something better. Recall that value in this state is 作者: atrophy 時間: 2025-3-24 07:21
A. D. Gardner,K. Richter,H. Rosemannxt.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: 粗魯性質(zhì) 時間: 2025-3-24 13:50
Bernhard Eisfeldxt.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: Rebate 時間: 2025-3-24 16:52 作者: 監(jiān)禁 時間: 2025-3-24 21:57
A. Krumbein,N. Krimmelbein,G. Schraufxt.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: OREX 時間: 2025-3-25 00:55
Andreas Michler,Ralf Heinrichxt.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: Glucocorticoids 時間: 2025-3-25 07:13 作者: 公司 時間: 2025-3-25 09:03 作者: assent 時間: 2025-3-25 15:02
Eike Hylla,Octavian Frederich,Johannes Mau?,Frank Thielext.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: 周興旺 時間: 2025-3-25 16:11
Christian Lübon,Manuel Kessler,Siegfried Wagnerxt.?..The book is essentialreading for planners, elected officials, developers, conservationists, andothers interested in the creation and maintenance of open space lands and urbangreen infrastructure projects or promoting a healthy economy...?.978-1-61091-693-6作者: GEM 時間: 2025-3-25 23:44 作者: asthma 時間: 2025-3-26 02:05
Conference proceedings 2010ersities, research-establishments and industry doing research and project work in numerical and experimental fluid mechanics and aerodynamics for aerospace and other applications. This has always been the basis of numerous common research activities sponsored by different funding agencies. Since 198作者: emission 時間: 2025-3-26 05:18 作者: DAUNT 時間: 2025-3-26 11:14
1612-2909 ce and other applications. This has always been the basis of numerous common research activities sponsored by different funding agencies. Since 198978-3-642-42252-2978-3-642-14243-7Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: Gene408 時間: 2025-3-26 14:14
ZhenLi Chen,Antoine Devesa,Stefan Hickel,Christian Stemmer,Nikolaus A. Adams作者: mutineer 時間: 2025-3-26 17:09 作者: ligature 時間: 2025-3-27 00:08
Application of the Multi-Scale-Finite-Volume Method to the Simulation of Incompressible Flows with Ilting Poisson equation is formally identical to the elliptic problems governing flows in porous media. An efficient iterative procedure for the computation of the pressure is then obtained by adapting the iterative-multi-scale-finite-volume procedure by Hajibeygi et al. [2].作者: Admonish 時間: 2025-3-27 03:57 作者: Cocker 時間: 2025-3-27 05:44 作者: Offensive 時間: 2025-3-27 12:46
Detached-Eddy Simulation of Supersonic Flow Past Cylindrical Aft Body with and without Base Bleedns based on RANS and experimental data for the base flow without bleed. To understand the influence of the bleed on the flow and the base pressure distribution, predictions of the base flow with bleed are compared with numerical data of the case without bleed.作者: 易改變 時間: 2025-3-27 17:26
Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR , Codeons during the ongoing flow computation. The procedure is applied to a three-dimensional wing-body configuration and the sensitivity of the coupled system to a variety of coupling parameters is investigated.作者: 憎惡 時間: 2025-3-27 18:33
An Approach to the Gust Problem with Interfering Profilesdy wake of the leading profile encounters the trailing profile and effects a load change. A first simplified attempt has been made using a rigid grid where both profiles execute a synchronous heaving motion.作者: Spartan 時間: 2025-3-28 00:20 作者: 仲裁者 時間: 2025-3-28 02:50
A Wall Model Based on Simplified Thin Boundary Layer Equations for Implicit Large Eddy Simulation ofsition between the simplified TBLE model and the LES should be located at the bottom of the logarithmic region. The grid resolution requirement depends mainly on the embedded TBLE grids and is only weakly dependent on the Reynolds number.作者: alleviate 時間: 2025-3-28 07:00 作者: esoteric 時間: 2025-3-28 12:07
Numerical Simulation of the Elastic and Trimmed Aircraft-structure interaction (FSI) procedure uses a partitioned approach to compute the flow around the configuration in static aeroelastic equilibrium. This simulation environment has been successfully applied to trim a rigid transportaircraft configuration in viscous flow as well as in inviscid flow with rigid and flexible wing.作者: adipose-tissue 時間: 2025-3-28 15:38
Turbulence Modeling and Detached Eddy Simulation with a High-Order Unstructured Discontinuous Galerkid method between the Unsteady Reynolds averaged Navier-Stokes approach and the Large Eddy Simulation. Some results, like flows over a flat plate and around a sphere, which could not be predicted with an Unsteady Reynolds averaged Navier-Stokes calculation, are calculated with high accuracy and compared with theory and experiments.作者: 馬具 時間: 2025-3-28 21:32
An Explicit Space-Time Discontinuous Galerkin Scheme with Local Time-Stepping for Unsteady Flowsand introducing local time-stepping and the shock capturing property, where we have adopted the artificial viscosity approach as described by Persson and Peraire to our STE-DG scheme. Thus, we try to resolve the shock within a few relatively large grid cells forming a narrow viscous profile by locally adding some amount of artificial viscosity.作者: 喊叫 時間: 2025-3-28 23:26 作者: Definitive 時間: 2025-3-29 04:01
1612-2909 This volume contains the papers presented at the 16 DGLR/STAB-Symposium held at the Eurogress Aachen and organized by RWTH Aachen University, Germany, November, 3 - 4, 2008. STAB is the German Aerospace Aerodynamics Association, founded towards the end of the 1970‘s, whereas DGLR is the German Socie作者: 點(diǎn)燃 時間: 2025-3-29 07:48
Interfacial Area Transport Equation in Statistical-Eulerian-Eulerian Simulations of Multiphase Flow exemplary application, the development of a spray injection IATE is discussed. This includes interfacial growth due to velocity gradients and a new IA detection term which resolves ambiguities with boundary conditions.作者: DIKE 時間: 2025-3-29 14:39
Modelling and Validation of Covariance Transport Equations for Large-Eddy-Simulation of Ternary, Tur. This work develops and test transport equations for these moments, which include a non-equilibrium model for the subgrid scale scalar dissipation and the subgrad scale scalar cross-dissipation rates. Mixing models are then used to particle ensembles which represent the FDFs with the required moments.作者: 殺菌劑 時間: 2025-3-29 18:55 作者: 珊瑚 時間: 2025-3-29 22:42 作者: 微塵 時間: 2025-3-30 01:54 作者: Dysplasia 時間: 2025-3-30 04:08
Application of the Multi-Scale-Finite-Volume Method to the Simulation of Incompressible Flows with Ie formulation proposed by Peller et al. [5]. In particular we derive exact constraints for the pressure at immersed solid walls and show that the resulting Poisson equation is formally identical to the elliptic problems governing flows in porous media. An efficient iterative procedure for the comput作者: WATER 時間: 2025-3-30 12:02 作者: Panther 時間: 2025-3-30 14:12 作者: handle 時間: 2025-3-30 18:50 作者: Adherent 時間: 2025-3-30 23:56
Application of a New Roughness Extension for ,???, Turbulence Modelsa flat plate and around the NACA 65.-215 airfoil with a rough surface. The results are compared to predictions using the boundary condition originally devised by Wilcox [11] for rough surfaces, and to predictions with the Spalart-Allmaras model with the Boeing roughness extension by Aupoix and Spala作者: 吼叫 時間: 2025-3-31 02:56
Improved Wall Functions Based on the 1D Boundary Layer Equations for Flows with Significant Pressureequations for wall-parallel velocity, including pressure gradient term and convective term, and turbulence quantities in wall normal direction. For each wall node, this system of equations is integrated numerically on an embedded subgrid between wall node and first node above the wall. The method is作者: employor 時間: 2025-3-31 06:10
A Wall Model Based on Simplified Thin Boundary Layer Equations for Implicit Large Eddy Simulation ofyer Equations (TBLE) is designed and applied to turbulent channel flow for a wide range of friction Reynolds numbers up to .. =20,000. The prediction capability of the employed wall model concerning mean velocities and Reynolds stresses is satisfactory, even on very coarse LES grids. The coupling po作者: Impugn 時間: 2025-3-31 10:57
Detached-Eddy Simulation of Supersonic Flow Past Cylindrical Aft Body with and without Base Bleed end, simulations are performed using detached-eddy simulation. To evaluate the performance of DES, numerical predictions are compared with computations based on RANS and experimental data for the base flow without bleed. To understand the influence of the bleed on the flow and the base pressure dis作者: 商品 時間: 2025-3-31 16:41
Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experimentde-wall. Results show that the effect of the sidewalls is similar to an offset in the angle of attack (but can only partially be corrected by a change in .), and that this effect is proportional to the lift and Mach number. These results were used in the design phase for the iGREEN wing-tailplane in作者: hurricane 時間: 2025-3-31 20:01
The Influence of the Length Scale Equation on the Simulation Results of Aerodynamic Flows Using Diffequation, have been applied to the transonic flow around the RAE 2822 airfoil and the ONERA M6 wing. Comparison with the Wilcox . – . model shows the influence of replacing the .-equation and the Boussinesq hypothesis by the modeled Reynolds stress transport equation. Particularly for the M6 wing di作者: 光明正大 時間: 2025-3-31 23:58
Efficient Flow Computation Including Turbulent Transportgrid framework. In previous investigations [7,8,10], the algebraic model of Baldwin and Lomax [1] was employed as turbulence model. In the present contribution, this model is replaced by the model of Spalart and Allmaras [9], where an additional partial differential equation has to be solved. The de作者: eucalyptus 時間: 2025-4-1 03:06
Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR , Codeien-Schlichting and cross-flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general aircraft configurations during the ongoing flow computation. The procedure is applied to a three-dimensional wing-body configuration and the sensitivity of the coupled sy作者: panorama 時間: 2025-4-1 09:58
Numerical Simulation of the Elastic and Trimmed Aircraftpled with a procedure to account for the interaction between fluid and structure. The trim algorithm is based on a Newton method with a discretized Jacobian. It incorporates the six degreesof- freedom (DoF) flight-mechanics equations and thereby enables to compute different trimmed states. The fluid作者: 我們的面粉 時間: 2025-4-1 13:58 作者: Focus-Words 時間: 2025-4-1 14:22 作者: OATH 時間: 2025-4-1 20:55
