咨询与建议

限定检索结果

文献类型

  • 183 篇 期刊文献
  • 15 篇 会议

馆藏范围

  • 198 篇 电子文献
  • 0 种 纸本馆藏

日期分布

学科分类号

  • 180 篇 工学
    • 127 篇 航空宇航科学与技...
    • 26 篇 仪器科学与技术
    • 20 篇 机械工程
    • 15 篇 计算机科学与技术...
    • 13 篇 力学(可授工学、理...
    • 8 篇 动力工程及工程热...
    • 8 篇 电气工程
    • 7 篇 土木工程
    • 7 篇 交通运输工程
    • 5 篇 化学工程与技术
    • 4 篇 石油与天然气工程
    • 3 篇 软件工程
    • 2 篇 光学工程
    • 2 篇 材料科学与工程(可...
    • 2 篇 信息与通信工程
    • 2 篇 控制科学与工程
    • 2 篇 矿业工程
    • 1 篇 冶金工程
    • 1 篇 电子科学与技术(可...
    • 1 篇 建筑学
  • 44 篇 管理学
    • 43 篇 管理科学与工程(可...
  • 32 篇 理学
    • 21 篇 数学
    • 11 篇 物理学
    • 3 篇 统计学(可授理学、...
    • 2 篇 化学
  • 5 篇 经济学
    • 5 篇 理论经济学
    • 2 篇 应用经济学
  • 1 篇 医学

主题

  • 198 篇 solution algorit...
  • 25 篇 angle of attack
  • 23 篇 navier stokes eq...
  • 16 篇 euler equations
  • 15 篇 unstructured gri...
  • 14 篇 pressure coeffic...
  • 13 篇 freestream mach ...
  • 12 篇 turbulence model...
  • 12 篇 computing
  • 11 篇 reynolds average...
  • 11 篇 lift coefficient
  • 10 篇 numerical simula...
  • 10 篇 continuity equat...
  • 9 篇 numerical algori...
  • 9 篇 numerical integr...
  • 9 篇 aspect ratio
  • 8 篇 earth
  • 8 篇 flow conditions
  • 7 篇 naca 0012
  • 7 篇 freestream condi...

机构

  • 3 篇 university of mi...
  • 2 篇 tech univ bergak...
  • 2 篇 sharif univ tech...
  • 2 篇 purdue universit...
  • 2 篇 calif state univ...
  • 2 篇 nasa langley res...
  • 2 篇 univ toronto ins...
  • 2 篇 nasa ames resear...
  • 2 篇 univ washington ...
  • 2 篇 nasa ames res ct...
  • 2 篇 texas a&m univ d...
  • 2 篇 univ pavia dipar...
  • 2 篇 tech univ bergak...
  • 2 篇 nasa langley res...
  • 2 篇 politecn torino ...
  • 2 篇 nasa ames resear...
  • 2 篇 mcdonnell aircra...
  • 2 篇 sharif univ tech...
  • 2 篇 european ctr tra...
  • 2 篇 michigan state u...

作者

  • 5 篇 batina jt
  • 5 篇 dempe stephan
  • 3 篇 yan shangyao
  • 3 篇 bernitsas mm
  • 3 篇 baysal o
  • 3 篇 zingg david w.
  • 2 篇 mclaren md
  • 2 篇 gagnon je
  • 2 篇 naghdabadi r.
  • 2 篇 reali a.
  • 2 篇 pelletier d
  • 2 篇 mersha ayalew ge...
  • 2 篇 stookesberry d
  • 2 篇 slater gl
  • 2 篇 verhoff a
  • 2 篇 auricchio f.
  • 2 篇 chieng cc
  • 2 篇 mathur sr
  • 2 篇 arghavani j.
  • 2 篇 drezner zvi

语言

  • 189 篇 英文
  • 9 篇 其他
检索条件"主题词=solution algorithm"
198 条 记 录,以下是111-120 订阅
排序:
Coupled ordinates method for multigrid acceleration of radiation calculations
收藏 引用
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER 1999年 第4期13卷 467-473页
作者: Mathur, SR Murthy, JY Fluent Inc Lebanon NH 03766 USA Carnegie Mellon Univ Dept Mech Engn Pittsburgh PA 15213 USA
The finite volume and discrete ordinates methods are known to converge increasingly slowly as the optical thickness is increased. This is a result of the sequential nature of the solution procedure;the equations for e... 详细信息
来源: 评论
Multiblock approach for calculating incompressible fluid flows on unstructured grids
收藏 引用
AIAA JOURNAL 1999年 第2期37卷 169-176页
作者: Sheng, CH Whitfield, DL Anderson, WK Mississippi State Univ Natl Sci Fdn Engn Res Ctr Computat Fluid Dynam Lab Mississippi State MS 39762 USA NASA Langley Res Ctr Aerodynam & Acoust Methods Branch Fluid Mech & Acoust Div Hampton VA 23681 USA
A multiblock approach is presented for solving two-dimensional incompressible turbulent Bows on unstructured grids. The artificial compressibility form of the governing equations Is solved by a node-based, finite volu... 详细信息
来源: 评论
Finite volume discretization aspects for viscous flows on mixed unstructured grids
收藏 引用
AIAA JOURNAL 1999年 第2期37卷 177-184页
作者: Haselbacher, A McGuirk, JJ Page, GJ Univ Loughborough Dept Aeronaut Engn Loughborough LE11 3TU Leics England
A solution method for compressible turbulent flows on unstructured grids in two dimensions is described. The method can be used on grids consisting of triangular and/or quadrilateral cells. Control volumes are constru... 详细信息
来源: 评论
Mean value analysis of military airlift operations at an individual airfield
收藏 引用
JOURNAL OF AIRCRAFT 1999年 第5期36卷 750-755页
作者: Dietz, DC USAF Inst Technol Dept Operat Sci Wright Patterson AFB OH 45433 USA
An analytical queueing network model of airlift operations at an individual airfield is developed and implemented. The airfield system is represented as a capacitated open network of multiserver queues and fork-join c... 详细信息
来源: 评论
Plastic analysis of complex microstructure composites using the generalized method of cells
收藏 引用
AIAA JOURNAL 1999年 第4期37卷 482-488页
作者: Orozco, CE Pindera, MJ Univ Virginia Dept Civil Engn Charlottesville VA 22903 USA
A recently developed computationally efficient implementation of the Generalized Method of Cells is extended here to deal with plasticity problems. The new formulation can be used to perform linear elastic and plastic... 详细信息
来源: 评论
Adaptive finite element solution of compressible turbulent flows
收藏 引用
AIAA JOURNAL 1998年 第12期36卷 2187-2194页
作者: Ilinca, F Pelletier, D Ignat, L Natl Res Council Canada Inst Ind Mat Boucherville PQ Canada Ecole Polytech Dept Mech Engn Montreal PQ H3C 3A7 Canada
An adaptive finite element method for solving compressible turbulent Bows up to transonic regime is presented. Pressure-based methods previously developed for laminar compressible Bows and turbulent incompressible flo... 详细信息
来源: 评论
Series load flow: A novel non-iterative load flow method
收藏 引用
IEE PROCEEDINGS-GENERATION TRANSMISSION AND DISTRIBUTION 1998年 第3期145卷 251-256页
作者: Xu, W Liu, Y Salmon, JC Le, T Chang, GWK Univ Alberta Dept Elect & Comp Engn Edmonton AB T6G 2G7 Canada Virginia Polytech Inst & State Univ Dept Elect Engn Blacksburg VA 24061 USA ABB Power T&D Co Inc Raleigh NC 27606 USA Siemens Power T&D LLC Brooklyn Pk MN 55428 USA
A noniterative method for solving load flow equations is presented in the paper. The method is based on the Taylor series expansion of the inverse load flow function. Formulas to compute the Taylor series are derived ... 详细信息
来源: 评论
Three-dimensional flow computation around a projectile overtaking a preceding shock wave
收藏 引用
JOURNAL OF SPACECRAFT AND ROCKETS 1998年 第5期35卷 619-625页
作者: Watanabe, R Fujii, K Higashino, F Tokyo Noko Univ Dept Mech Syst Engn Tokyo Japan Inst Space & Astronaut Sci Kanagawa 229 Japan
A numerical simulation of the flowfield around a projectile overtaking a preceding shock wave is carried out by solving the three-dimensional, thin layer Navier-Stokes equations. A domain decomposition method with the... 详细信息
来源: 评论
Assessment of a radiative heat transfer model for gas turbine combustor preliminary design
收藏 引用
JOURNAL OF PROPULSION AND POWER 1998年 第1期14卷 66-73页
作者: Stuttaford, PJ Rubini, PA Cranfield Univ Sch Mech Engn Bedford MK43 0AL England
The early stages of gas turbine combustor design represent a challenging combination of analytical analysis, numerical simulation, and rig testing. The objective of this work is the development of a versatile radiatio... 详细信息
来源: 评论
Damped oscillations of a liquid/gas surface upon step reduction in gravity
收藏 引用
JOURNAL OF SPACECRAFT AND ROCKETS 1997年 第1期34卷 110-117页
作者: Wolk, G Dreyer, M Rath, HJ Weislogel, MM NASA LEWIS RES CTRMICROGRAV FLUIDS BRANCHCLEVELANDOH 44135
The reorientation and settling of a liquid/gas interface in a right circular cylinder upon step reduction in gravity is investigated numerically. A modified dynamic contact angle boundary condition is implemented wher... 详细信息
来源: 评论