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Ryoichi Takahashi
Dept. of Mechanical Engineering, Tokyo Institute of Technology Ohkayama, Meguro-ku, Tokyo 110, Japan

Kiyoshi Matsubara
Reseaach and Engineering Technology Div. Fuji Research Institute Corp. 3-2-12, Kaigan, Minato-ku, Tokyo 108, Japan

Hideaki Koike
Research and Engineering Technology Div. Fuji Research Institute Corp. 3-2-12, Kaigan, Minato-ku, Tokyo 108, Japan


Basically the numerical simulation consists of modeling, transformation, computation and understanding the resulting data. These four processes should be reinforced by such three feedback as validation of the mathematical models and verification of both the difference-schemes and the computer programs. Technically the quality of the numerical solution or the simulation cost depends highly on a decrease in degree of the four errors of modeling, measurement, truncation and round off.
The fully-experienced engineer and/or beginner shall hesitate to conduct the computation of the given heat and mass transfer problem until the numerical difficulties are removed from the simulation procedures. Introduction of a expert system may be a solution for the complicated flow problems of the design-base.
This paper will demonstrate that the present consultative expert system for a advanced cfd code, α-FLOW, is examined and found feasible after careful implementations.

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Bow shocks on a jet-like solid body shape. Thermal Sciences 2004, 2004. Pulsed, supersonic fuel jets - their characteristics and potential for improved diesel engine injection. PULSED, SUPERSONIC FUEL JETS - THEIR CHARACTERISTICS AND POTENTIAL FOR IMPROVED DIESEL ENGINE INJECTION
View of engine compartment components (left). Plots of temperature distributions in centreplane, forward of engine (right). CHT-04 - Advances in Computational Heat Transfer III, 2004. Devel... DEVELOPMENT AND CURRENT STATUS OF INDUSTRIAL THERMOFLUIDS CFD ANALYSIS
Pratt & Whitney's F-135 Joint Strike Fighter Engine under test in Florida is a 3600F class jet engine. TURBINE-09, 2009. Turbine airfoil leading edge stagnation aerodynamics and heat transfe... TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW
Refractive index reconstructed field. (a) Second iteration. (b) Fourth iteration. Radiative Transfer - VI, 2010. Theoretical development for refractive index reconstruction from a radiative ... THEORETICAL DEVELOPMENT FOR REFRACTIVE INDEX RECONSTRUCTION FROM A RADIATIVE TRANSFER EQUATION-BASED ALGORITHM
Two inclusion test, four collimated sources. Radiative Transfer - VI, 2010. New developments in frequency domain optical tomography. Part II. Application with a L-BFGS associated to an inexa... NEW DEVELOPMENTS IN FREQUENCY DOMAIN OPTICAL TOMOGRAPHY. PART II. APPLICATION WITH A L-BFGS ASSOCIATED TO AN INEXACT LINE SEARCH