標(biāo)題: Titlebook: Sixteenth International Conference on Numerical Methods in Fluid Dynamics; Proceedings of the C Charles-Henri Bruneau Conference proceeding [打印本頁(yè)] 作者: 無(wú)法生存 時(shí)間: 2025-3-21 19:35
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics影響因子(影響力)
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics影響因子(影響力)學(xué)科排名
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics網(wǎng)絡(luò)公開度
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics被引頻次
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics被引頻次學(xué)科排名
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics年度引用
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics年度引用學(xué)科排名
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics讀者反饋
書目名稱Sixteenth International Conference on Numerical Methods in Fluid Dynamics讀者反饋學(xué)科排名
作者: 廣告 時(shí)間: 2025-3-21 23:59
G. Carré,L. Fournier,S. Lanteril layers) are detailed;..? chapters 5 to 8 focus on studies of light scattering by single particles and radially inhomogeneous media;..? the final chapter discusses the environmental polarimetry of man-made objects..978-3-662-57015-9978-3-662-49538-4作者: 花束 時(shí)間: 2025-3-22 03:51 作者: 乞丐 時(shí)間: 2025-3-22 08:24 作者: deriver 時(shí)間: 2025-3-22 10:37
Yoko Takakura,Takayoshi Suzuki,Fumio Higashino,Masahiro Yoshida作者: Generosity 時(shí)間: 2025-3-22 15:12
X. Y. Wang,S. C. Chang,K. H. Kao,Ph. Jorgenson,C. Y. Chow作者: nitroglycerin 時(shí)間: 2025-3-22 20:09
Aspects (and aspect ratios) of cartesian mesh methods,作者: 過(guò)份好問(wèn) 時(shí)間: 2025-3-22 21:35 作者: 不如樂(lè)死去 時(shí)間: 2025-3-23 02:16 作者: 啞巴 時(shí)間: 2025-3-23 07:00 作者: Allure 時(shí)間: 2025-3-23 12:53 作者: 蚊子 時(shí)間: 2025-3-23 14:36
A. Dadone,B. Grossmanlevant theoretical technique. The small-amplitude perturbation theory was one of the earlier theories used, it was originally developed by Rice. .This theory still remains of interest.,.-. because perturbative terms of order higher than one can produce enhanced backscattering or improve the accuracy作者: Jocose 時(shí)間: 2025-3-23 21:33
Denis Darracq,Steeve Champagneux,Alexandre Corjonar-field images strongly depend on the specific properties of each tip. It cannot be assumed in general that the signal delivered by a near-field scanning microscope delivers a signal proportional to the square of the local electric field. In the last part of the paper, we derive from the reciprocit作者: –LOUS 時(shí)間: 2025-3-24 01:23 作者: 貧窮地活 時(shí)間: 2025-3-24 02:39 作者: Vo2-Max 時(shí)間: 2025-3-24 07:51
978-3-662-14177-9Springer-Verlag Berlin Heidelberg 1998作者: Biofeedback 時(shí)間: 2025-3-24 12:50
Sixteenth International Conference on Numerical Methods in Fluid Dynamics978-3-540-49540-6Series ISSN 0075-8450 Series E-ISSN 1616-6361 作者: Flu表流動(dòng) 時(shí)間: 2025-3-24 16:31
Multigrid by agglomeration for the acceleration of compressible flow calculations on unstructured mWe describe ongoing research activities at . Sophia Antipolis aiming at the construction of efficient and robust unstructured multigrid solvers for complex 2D and 3D flow simulations.作者: 你正派 時(shí)間: 2025-3-24 22:07 作者: GOAT 時(shí)間: 2025-3-25 00:16
Efficient calculation of 3-D turbulent transonic flows, technique. The scheme is driven to steady-state by various implicit treatments, the pros and cons of which are discussed in terms of cost and memory requirement. The efficiency and accuracy of the proposed methods are assessed by computing transonic flows over wings.作者: archaeology 時(shí)間: 2025-3-25 07:24 作者: 粘連 時(shí)間: 2025-3-25 08:11 作者: 精密 時(shí)間: 2025-3-25 15:34
Conference proceedings 1998mputational modeling of partial differential equations pertinent primarily to aeronautical applications. The reader will find five survey articles on cartesian mesh methods, on numerical studies of turbulent boundary layers, on efficient computation of compressible flows, on the use of Riemann-solvers and on numerical procedures in complex flows.作者: Nerve-Block 時(shí)間: 2025-3-25 16:17
Lecture Notes in Physicshttp://image.papertrans.cn/s/image/868148.jpg作者: 小卒 時(shí)間: 2025-3-25 22:56
https://doi.org/10.1007/BFb0106552calculus; fluid dynamics; modeling; numerical methods; partial differential equation; fluid- and aerodyna作者: 壕溝 時(shí)間: 2025-3-26 00:57 作者: CYT 時(shí)間: 2025-3-26 05:32
Approximation of compressible flows by a reduced order model,D). The POD basis functions are used to filter, at each time step, the solution obtained from a finite-volume code. Three test cases are discussed: unsteady Euler flow about an oscillating airfoil, laminar vortex shedding from a NACA-0012 airfoil at incidence, and finally turbulent vortex shedding from a square cylinder.作者: 尊重 時(shí)間: 2025-3-26 12:13 作者: Fatten 時(shí)間: 2025-3-26 12:38
A supersonic inverse wing design method and its application to Japanese SST, of . .=2.0. Several design constraints need to be satisfied. By means of the method, a wing has been designed which has desirable aerodynamic characteristics while using only a small amount of computation time.作者: Albinism 時(shí)間: 2025-3-26 19:42 作者: IVORY 時(shí)間: 2025-3-26 22:36 作者: 激怒 時(shí)間: 2025-3-27 02:40 作者: Gastric 時(shí)間: 2025-3-27 05:46 作者: glacial 時(shí)間: 2025-3-27 13:04 作者: GLUE 時(shí)間: 2025-3-27 15:46 作者: Mosaic 時(shí)間: 2025-3-27 20:41 作者: 符合規(guī)定 時(shí)間: 2025-3-28 00:41
0075-8450 ticles on cartesian mesh methods, on numerical studies of turbulent boundary layers, on efficient computation of compressible flows, on the use of Riemann-solvers and on numerical procedures in complex flows.978-3-662-14177-9978-3-540-49540-6Series ISSN 0075-8450 Series E-ISSN 1616-6361 作者: 不可侵犯 時(shí)間: 2025-3-28 04:09 作者: indicate 時(shí)間: 2025-3-28 08:59
0075-8450 sted in computational modeling of partial differential equations pertinent primarily to aeronautical applications. The reader will find five survey articles on cartesian mesh methods, on numerical studies of turbulent boundary layers, on efficient computation of compressible flows, on the use of Rie作者: habitat 時(shí)間: 2025-3-28 11:36
Conference proceedings 1998mputational modeling of partial differential equations pertinent primarily to aeronautical applications. The reader will find five survey articles on cartesian mesh methods, on numerical studies of turbulent boundary layers, on efficient computation of compressible flows, on the use of Riemann-solve作者: 口味 時(shí)間: 2025-3-28 17:58
Efficient calculation of 3-D turbulent transonic flows, technique. The scheme is driven to steady-state by various implicit treatments, the pros and cons of which are discussed in terms of cost and memory requirement. The efficiency and accuracy of the proposed methods are assessed by computing transonic flows over wings.作者: SEVER 時(shí)間: 2025-3-28 21:47 作者: 乏味 時(shí)間: 2025-3-28 23:11
Time-accurate fluid-structure coupling for turbulent flows,ulent transonic flows around airfoils in arbitrary motion. The resolution of the structural system resolution is performed with an unconditionnally stable algorithm. Computations of two test cases with forced oscillation and one with flutter are analyzed.作者: 充氣女 時(shí)間: 2025-3-29 03:23 作者: Distribution 時(shí)間: 2025-3-29 09:30
Hybrid-cartesian grid procedure for the simulation of compressible turbulent flows,h made of general polygonal elements is obtained by intersecting hyperbolic grids generated in the boundary layers and in the wakes with a Cartesian grid covering the whole domain of computation. The flow solver is based on a cell-centered high-order finite volume scheme. A multigrid preconditioned 作者: acetylcholine 時(shí)間: 2025-3-29 13:06 作者: Nibble 時(shí)間: 2025-3-29 16:03
Numerical simulations of two blasts by a supersonic projectile discharged from a tube,ube into ambient air. The Euler equations, assuming axisymmetric flows, were solved using a dispersion-controlled scheme implemented with moving boundary conditions. The numerical results show that not only does the leading shock due to the second blast overtake the projectile but also the gas behin作者: Myocyte 時(shí)間: 2025-3-29 23:42
Numerical study of effects of a bellmouth on the entrance pipe flow, Until now, the axial velocity has been assumed to be uniform at the bellmouth outlet. The calculation results, however, reveal that it develops a profile somewhat towards the Poiseuille’s parabolic profile. Moreover, a feasible reason for the increase in critical Reynolds number when using bellmout作者: 調(diào)色板 時(shí)間: 2025-3-30 03:15
A fast, matrix-free implicit method for compressible flows on unstructured grids,e system of linear equations arising from the Newton linearization is solved by the GMRES (Generalized Minimum RESidual) algorithm with a LU-SGS (Lower-Upper Symmetric Gauss-Seidel) preconditioner. A remarkable feature of the present GMRES+LU-SGS method is that the storage of the Jacobian matrix can作者: 長(zhǎng)矛 時(shí)間: 2025-3-30 07:48
A supersonic inverse wing design method and its application to Japanese SST,r has been devised. The method handles SST wing-fuselage configurations and provides the wing section geometry at every span station. It uses the inverse problem solver and Navier-Stokes simulation. The design target is a natural laminar flow (NLF) wing for the wing-fuselage combination at the speed作者: diathermy 時(shí)間: 2025-3-30 09:58 作者: Organonitrile 時(shí)間: 2025-3-30 15:10 作者: 吞下 時(shí)間: 2025-3-30 17:11 作者: 繼承人 時(shí)間: 2025-3-31 00:42 作者: DEVIL 時(shí)間: 2025-3-31 03:31 作者: 粗糙 時(shí)間: 2025-3-31 06:59 作者: palliate 時(shí)間: 2025-3-31 12:30 作者: 來(lái)就得意 時(shí)間: 2025-3-31 16:42 作者: Nostalgia 時(shí)間: 2025-3-31 20:56 作者: 真 時(shí)間: 2025-4-1 00:53 作者: Ganglion-Cyst 時(shí)間: 2025-4-1 03:59 作者: AVERT 時(shí)間: 2025-4-1 07:47 作者: 值得贊賞 時(shí)間: 2025-4-1 13:25
S. Edwards,J. Reuther,J. J. Chattotn microscopy. These fragments associate with phospholipids. The fragments/lipid association is named a Biovector and can be used as a drug delivery system or in vaccine formulations..Light scattering reveals that the fragments are spheres with R.≈ 50 nm. Under some experimental conditions (namely, h作者: heckle 時(shí)間: 2025-4-1 15:19
Philippe Geuzaine,Jean-André Essersrtical and horizontal profiles obtained in summer with aircraft flights. Aerosol size data has been obtained with diffusion batteries, electrostatic precipitators, and cascade impactors..There is a strong (5 to 1) seasonal variation in surface aerosol concentrations, with the maximum aerosol concent作者: 埋伏 時(shí)間: 2025-4-1 21:37
Front Matteredingungen, eine sehr gro?e praktische Bedeutung erlangt. Durch den Einsatz leistungselektronischer Speisung werden kontinuierlich neue Anwendungen in geregelten Antrieben erschlossen. Die Nutzung als Generator in Windenergieanlagen ist ein aktuelles Beispiel..Wegen der in vielerlei Hinsicht untersc作者: MORPH 時(shí)間: 2025-4-2 01:02
