The primary purpose of the FLOMANIA proposal was to support the European aeronautics
community (industry, research labs and universities) in the area of flow physics modelling by …

This chapter describes the use of computational fluid mechanics at Dassault Aviation. A
historical perspective gives a measure of the successive giant steps that have been made …

This paper presents validation test cases of an LES solver based on an unstructured finite-
element compressible Navier-Stokes code. After a short description of the industrial tool, we …

Abstract This chapter covers Dassault Aviation's contribution to Workpackage 3 of the
ADIGMA Project, which focuses on the extension of its stabilized finite element industrial …

An integrated scramjet experiment is proposed as an" Integration Validation Object." A
model was tested in different facilities at ITAM with and without combustion. The behavior of …

NNFM 128 - Higher-Order RANS and DES in an Industrial Stabilized Finite Element Code
Page 1 Higher-Order RANS and DES in an Industrial Stabilized Finite Element Code F …

In this Section a detailed and quantitative understanding is provided of how algorithms
should be designed and implemented to effectively target a range of existing and emerging …

This paper describes the extension of Dassault Aviation's stabilized finite element industrial
Navier-Stokes code to higher-order elements. The high-order approach is carefully …

In preparation for design studies of lifting body type aircrafts, Dassault Aviation and NLR
conducted a preliminary evaluation of the level ofCFD required for the prediction of the …

Abstract This chapter describes Dassault Aviation's contribution to Workpackage 5 of the
ADIGMA Project. The adjoint operator developed in the framework of optimum design is …