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C. Robin
Centre de Thermique de PINSA de Lyon - URA CNRS 1372 Laboratoire Equipement de l'Habitat Bat 307 INSA; and O.C.G.R. Ing%nierie, 129, chemin Moulin Carron, BP 95, F69136 ECULLY C6dex, FRANCE

F. Allard
Centre de Thermique de PINSA de Lyon - URA CNRS 1372 Laboratoire Equipement de l'Habitat Bat 307 INSA, 20 avenue Albert Einstein, F69621 Villeurbanne Cedex, FRANCE

J. Brau
INSA LYON, CETHIL, Bat 307, Av Albert Einstein 69621 Cedex, Villeurbanne, France

R. Velazquez
Departamento de Ingenieria Energetica y Fluidomecanica, Universidad de Sevilla, Avda Reina Mercedes S/N, 41012 Sevilla, SPAIN


SETIS is a computer support for thermal design of buildings. Since the initial stages of the design process, it deals both with the envelope of building and with its HVAC system. This project is managed by OCGR, a french civil engineering office, and Laboratoire Equipement de l'Habitat de 1TNSA de LYON. This collaboration is very important because SETIS is defined as a tool which integrates both algorithmic programs and knowledge based parts. They both work on the same database where a thermal description of the building to design is stored. The second aspect of SETIS is its decision-making ability : a Supervisor can suggest to the designer modifications or actions in order to keep the description of his project consistent.

ICHMT Digital Library

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