Distributed-Memory Computing With the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA)

نویسندگان

  • Christopher J. Riley
  • F. McNeil Cheatwood
چکیده

The Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA), a NavierStokes solver, has been modi ed for use in a parallel, distributed-memory environment using the Message-Passing Interface (MPI) standard. A standard domain decomposition strategy is used in which the computational domain is divided into subdomains with each subdomain assigned to a processor. Performance is examined on dedicated parallel machines and a network of desktop workstations. The e ect of domain decomposition and frequency of boundary updates on performance and convergence is also examined for several realistic con gurations and conditions typical of large-scale computational uid dynamic analysis.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Characteristics of the Shuttle Orbiter Leeside Flow During A Reentry Condition

A study of the leeside ow characteristics of the Shuttle Orbiter is presented for a reentry ight condition. The ow is computed using a point-implicit, nite-volume scheme known as the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA). LAURA is a second-order accurate, laminar NavierStokes solver, incorporating nite-rate chemistry with a radiative equilibrium wall temperature distribu...

متن کامل

AIAA 2004–0612 A Structured-Grid Quality Measure for Simulated Hypersonic Flows

A structured-grid quality measure is proposed, combining three traditional measurements: intersection angles, stretching, and curvature. " Quality " assesses whether the grid generated provides the best possible trade-offs in grid stretching and skewness that enable accurate flow predictions, whereas the grid density is assumed to be a constraint imposed by the available computational resources...

متن کامل

AIAA 98-2575 Multi-Component Diffusion with Application To Computational Aerothermodynamics

The accuracy and complexity of solving multicomponent gaseous diffusion using the detailed multicomponent equations, the Stefan-Maxwell equations, and two commonly used approximate equations have been examined in a two part study. Part I examined the equations in a basic study with specified inputs in which the results are applicable for many applications. Part II addressed the application of t...

متن کامل

AIAA 98 - 2850 Mars Ascent Vehicle Flight Analysis

The scientific objective of the Mars Surveyor Program 2005 mission is to return Mars rock, soil, and atmospheric samples to Earth for detailed analysis. The present investigation focuses on design of Mars Ascent Vehicle for this mission. Aerodynamic, aerothermodynamic, and trajectory design considerations are addressed to assess the ascent configuration, determine aerodynamic stability, charact...

متن کامل

Aiaa 98-2850 Mars Ascent Vehicle Flight Analysis Mars Ascent Vehicle Flight Analysis

The scientific objective of the Mars Surveyor Program 2005 mission is to return Mars rock, soil, and atmospheric samples to Earth for detailed analysis. The present investigation focuses on design of Mars Ascent Vehicle for this mission. Aerodynamic, aerothermodynamic, and trajectory design considerations are addressed to assess the ascent configuration, determine aerodynamic stability, charact...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 1997