Computational aerodynamics based on the Euler equations: = L'aérodynamique numérique à partir des équations d'Euler

257 Pages·1994·49.23 MB·English

by  Slooff J. W.

AGARD-AG-325
ADVISORYGROUPFORAEROSPACERESEARCHlkDEVELOPMENT
7 RUE ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE
AQARDograph 325
Computational Aerodynamics Based
on the Euler Equations
(L’aeodynamique numerique B partir des
equations d’Euler)
This AGARLloxraph has been produced at the reauest of the Fluid DyMmics Panel (FDP)o f
AGARD.
NORTH ATLANTIC TREATY ORGANIZA’I ivn
I
Published September 1994
Distribution and Avai7ability on Back Cover
;

AGARD-AG-325
ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT
7 RUE ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE
AGARDograph 325
Computational Aerodynamics Based
on the Euler Equations
(L’aerodynamique numCrique B partir des
Cquations d’Euler)
Edited by
J.W. SLOOFF
National Aerospace Laboratory NLR
Anthony Fokkerweg 2
1059 CM Amsterdam
Netherlands
and
Dr. W. SCHMIDT
Air Vehicle Engineering
Military Aircraft Division
Deutsche Aerospace
8 1663 Munchen
Germany
This AGARDograph has been produced at the request of the Fluid Dynamics Panel (FDP) of
AGARD.
North Atlantic Treaty Organization
Organisation du fraifed e I’Aflanfique Nord
I
The Mission of AGARD
According to its Charter, the mission of AGARD is to bring together the leading personalities of the NATO nations in the
fields of science and technology relating to aerospace for the following purposes:
-R ecommending effective ways for the member nations to use their research and development capabilities for the
common benefit of the NATO community;
- Providing scientific and technical advice and assistance to the Military Committee in the field of aerospace research
and development (with particular regard to its military application);
- Continuously stimulating advances in the aerospace sciences relevant to strengthening the common defence posture;
- Improving the co-operation among member nations in aerospace research and development;
- Exchange of scientific and technical information;
- Providing assistance to member nations for the purpose of increasing their scientific and technical potential;
-Rendering scientific and technical assistance, as requested, to other NATO bodies and to member nations in
connection with research and development problems in the aerospace field.
The highest authority within AGARD is the National Delegates Board consisting of officially appointed senior
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Participation in AGARD activities is by invitation only and is normally limited to citizens of the NATO nations.
The content of this publication has been reproduced
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Published September 1994
Copyright 0 AGARD 1994
All Rights Reserved
ISBN 92-836-1005-9
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iv
Foreward and Introduction
Computational Fluid Dynamic (CFD) methods based on the Euler equations have been a subject of intensive research and
development over the past 10 to 15 years. They have now reached a stage where applications are an almost routine matter in
most aerospace industries, research laboratories and universities.
After the pioneering work of Lax and Wendroff in the early sixties there was a first, relatively short burst of activities
involving Euler methods in the late sixties and early seventies. These activities were closely related to the reviving interest in
transonic flow and supercritical wing technology in particular; they were soon to be overtaken by developments in transonic
potential flow methods triggered by the work of Murman and Cole.
The main reasons for this shift of attention were an apparent lack of robustness of the Euler methods that had evolved so far
but in particular the fact that potential flow methods offered an almost order-of-magnitude reduction of computational effort.
Given the level of computer technology at the time, the latter was mandatory if computational transonics were to become a
practical tool for the aerospace industry.
While the concentrated efforts on transonic potential flow methods of the seventies and early eighties led to widespread use
of such methods in aerospace applications,* a revival of interest in Euler methods was bound to happen and indeed did take
place around 1980, in particular through the interest created by the works of Rizzi and Jameson. The main driving factors for
this revival were:
- the inherent limitations of potential flow theory, in particular the inability to model vorticity;
-the fact that computer power had increased by a factor 10 to 15 since around 1970;
-the fact that a new generation of more efficient discretization schemes and algorithms held promise for future
practical applications.
Research on discretization schemes and algorithms for the Euler equations continues today; not in the least because of the
fact that the convective (i.e. “Eu1er”-) fluxes play a dominant role in CFD methods at the next highest level in mathematical
flow modeling, that is, the Navier-Stokes equations. At the same time however, Euler “codes” have reached a level of
proliferation in the aerospace aerodynamic community that justifies a review of the state of the art. It is worth noting that
Euler methods not only are being used for the simulation of flows for which the modeling of vorticity is mandatory, such as
leading-edge vortex flows and flows involving propulsion simulation, but that they are also being used for non-vortical flows
around complex geometries, since transonic potential flow methods for complex configurations did not fully mature.
The objective of this AGARDograph, then, is to provide a survey of the state-of-the-art in Computational Aerodynamics
Based on the Euler Equations. In terms of technology application, it concentrates on the numerical simulation of external
flows about aerospace vehicles.
Internal flows and turbomachinery applications are not extensively treated but touched upon where considered appropriate. In
terms of “audience” this AGARDograph is, in the first place, aimed at the applied computational aerodynamicist who wants
to get started in this field. However, it might also assist the aerodynamic engineering manager in judging whether his CFD-
tools are sufficiently “state-of-the-art” and, if not, in what direction improvement or extension of capabilities shoud be
sought. Finally, it might also help the research community to identify niches for further research. For those readers who
would like to consult basic text books on CFD and Euler methods, some general references are suggested at the end of this
Foreword and Introduction.
Chapter 1 is intended to provide a background of the fluid and thermodynamic theory required for understanding the physics
modelled by the Euler equations. Chapter 2 describes numerical schemes and algorithms. Although this is done from a CFD
specialist’s point of view, the reader should be able to identify the algorithm descriptions given in this chapter with the
methods given in the following chapter. In order to meet the objectives for this report, it was felt that the core of the
AGARDograph should consist of a survey and description of numerical schemes and algorithms, capabilities, and limitations
of the major Euler codes that are currently in use in the NATO countries. For that purpose, requests for information were sent
to institutions, industries and individuals who, to the authors’ knowledge, were or had been active in this area. The response
has been collected in Chapter 3, with examples of application given in Chapter 4.
* A survey can be found in AGARDograph 266 “Applied Computational Transonic Aerodynamics” by T. Holst, et al. 1982.
V
The preparation of this AGARDograph has been a team effort involving scientists from both Europe and North America.
Each of the authors contributed to several if not all of the chapters. In addition, each author took responsibility for
coordinating the efforts for the following:
Chapter 1 Nigel Weatherill
Chapter 2 Philippe Morice
Chapter 3 Herbert Rieger and Wolfang Schmidt
Chapter 4 Jim Thomas and Kyle Anderson
Writing it and putting it all together was a substantial amount of work. We thank the authors for their efforts and enthusiasm
and their organisations for making it possible.
We also thank all the individuals from the NATO countries that provided material to the authors. Without their help this
AGARDograph would have been less complete.
Joop Slooff,
Wolfgang Schmidt
Editors,
Fluid Dynamics Panel
General References
1. Hirsch, Ch. “Numerical Computation of Internal and External Flows”, Vols. 1 & 2. John Wiley & Sons Ltd., 1988/90.
ISBN 0 471 91762 1/0 471 92351 6.
2. Eberle, A., Rizzi, A., Hirshel, E.H., “Numerical Solutions of the Euler Equations for Steady Flow Problems”, Notes on
Numerical Fluid Dynamics, Vol. 34 Vieweg, BraunschweiglWiesbaden, 1991.
vi
Avant-propos et introduction
Les mtthodes de I’atrodynamique numtrique (CFD) bastes sur les tquations d’Euler ont fait l’objet de recherches et
dtveloppement intensifs depuis une quinzaine d’anntes. Aujourd’hui ces mtthodes sont appliqutks de faGon quasi-courante,
dans la plupart des industries aerospatiales, des laboratoires de recherche et des universitts.
Les travaux d’avant-garde de Lax et Wendroff du dtbut des anntes soixante ont ttt suivis d’une premitre ptriode d’activitts,
relativement courte, concernant les mtthodes d’Euler, & la fin des anntes soixante et au dtbut des anntes soixante-dix. Ces
activitts ttaient ttroitement litks au regain d’inttrst qu’il y avait h l’gpoque pour les tcoulements transsoniques et les
technologies de profil d’aile supercritique en particulier. Cependant, elles furent rapidement dCpasstes par le dtveloppement
des methodes de calcul des Ccoulements potentiels transsoniques engendrtes par les travaux de Murman et Cole.
Les principales raisons de ce changement de direction furent le manque de robustesse apparent des mtthodes d’Euler de
1’Cpoque et en particulier le fait que les mtthodes de calcul des tcoulements potentiels permettaient la rauction du temps de
calcul d’environ un ordre de grandeur. Considtrant le niveau des technologies de l’informatique & l’tpoque, cette rgduction
s’imposait si l’on voulait que I’atrodynamique transsonique numCrique puisse devenir un outil pratique pour I’industrie
atrospatiale.
fitant donne que les efforts consacrts aux mtthodes de calcul des houlements potentiels transsoniques dans les anntes
soixante-dix et au dtbut des anntes quatre-vingts ont conduit A la banalisation de ces mtthodes dans les applications
aerospatiales, un regain d’inttrEt pour les mtthodes d’Euler ttait inevitable et ceci s’est produit en 1980, grace, en particulier,
& l’inttrst suscitt par les travaux de Rizzi et Jameson. Les principaux tltments moteur de ce renouveau furent :
- les limitations propres & la thtorie de I’tcoulement potentiel et, en particulier, la non-faisabilitt de la modtlisation du
rotationnel;
- le fait que la puissance de calcul avait augment6 d’un facteur de l’ordre de 10 & 15 depuis 1970;
- le fait qu’une nouvelle gtntration de mtthodes de discretisation et d’algorithmes plus efficaces semblaient promettre
des applications pratiques h I’avenir.
Les travaux de recherche sur les mtthodes de discrttisation et les algorithmes pour les equations d’Euler se poursuivent
aujourd’hui, principalement h cause du fait que les flux convectifs (c’est-h-dire ad’Eulen,) jouent un r61e prtdominant dans
les mtthodes de I’aCrodynamique numtrique au niveau immuiatement suptrieur de la modtlisation mathtmatique de
I’tcoulement, c’est-&-direa u niveau des Cquations Navier-Stokes. Paralltlement A ces dtveloppements pourtant, les cccodesw
Euler ont atteint un niveau de proliftration au sein de la communautt de l’atrodynamique atrospatiale qui justifie une revue
de l’6tat de l’art.
I1 convient de noter, ici, que les mtthodes d’Euler ne sont pas utilistes uniquement pour la simulation d’6coulements pour
lesquels la modtlisation du rotationnel est obligatoire, tels que les tcoulements tourbillonnaires de bord d’attaque et les
Ccoulements avec simulation de la propulsion car, en raison du fait que les mtthodes de calcul des Ccoulements potentiels
transsoniques ne sont jamais arrivtes A maturitb, les codes d’Euler sont utilists aussi pour les Ccoulements non
tourbillonnaires autour de gtomttries complexes.
L’objectif de cette AGARDographie est, donc, de donner un apequ de l’ttat de l’art dans le domaine de I’atrodynamique &
partir des equations d’Euler. En matitre d’application de la technologie l’accent est mis sur la simulation numtrique
d’tcoulements externes autour de vthicules atrospatiaux. Les flux internes et les applications turbomachines ne sont pas
traitts en profondeur, mais simplement abordCs, le cas hhtant.
En matitre de ccpublic,,, cette AGARDographie est destinte, en premier lieu, h I’atrodynamicien concern6 par le CFD qui
souhaite se familiariser avec ce domaine. Cependant, elle est susceptible d’inttresser aussi le manager d’Ctude et de
conception en matikre d’atrodynamique de gtnie atrodynamique et de lui faire savoir si ses outils CFD correspondent &
ccl’ttat de l’art, ou sinon, quelles sont les amtliorations et quelles sont les nouvelles capacitts & rechercher. Enfin, elle
pourrait apporter une aide & la communaute des chercheurs dans l’identification de projets futurs. Pour ceux qui
souhaiteraient consulter des ouvrages de caractte gtntral sur I’atrodynamique numtrique et les mtthodes d’Euler, un certain
nombre de rtftrences sont propostes h la fin de cette Introduction et avant-propos.
vii
Le chapitre 1 prtsente l’essentiel de la thtorie de la thermodynamique et des fluides ntcessaire h la comprthension de la
physique modelte par les tquations d’Euler. Le chapitre 2 donne la description de mtthodes numtriques et d’algorithmes.
Bien que cette description soit donnte du point de vue du sptcialiste CFD, le lecteur devrait pouvoir identifier les descriptions
des algorithmes donntes dans ce chapitre en se servant des mtthodes donntes dans le chapitre suivant. Compte tenu de ces
objectifs, les auteurs partageaient l’avis que l’essentiel de 1’AGARDographie devait consister en un tour d’horizon et un
descriptif des theories numtriques et des algorithmes, ainsi que des capacitts et des limitations des principaux codes d’Euler
actuellement utilises par les pays membres de I’OTAN. Ayant cet objectif en we, des demandes ont ttt adresstes aux
Ctablissements, aux industries et aux particuliers, qui, h la connaissance des auteurs, ttaient, ou avaient ttt actifs dans ce
domaine. Les rtponses obtenues sont expostes au chapitre 3, avec des exemples d’applications au chapitre 4.
La rtdaction de cette AGARDographie a ttt un vtritable travail d’tquipe, mobilisant des scientifiques de ]’Europe et de
1’AmCrique du Nord. Chacun des auteurs a contribut h plusieurs, sinon h I’ensemble des chapitres. En outre, chaque auteur
ttait responsable de la coordination des efforts consacrts h un chapitre en particulier, come suit :
Chapitre 1 Nigel Weatherill
Chapitre 2 Philippe Morice
Chapitre 3 Herbert Rieger et Wolfang Schmidt
Chapitre 4 Jim Thomas et Kyle Anderson
La rtdaction et la mise en forme ont represent6 un travail considerable. Nous tenons h remercier les auteurs de leurs efforts et
leur enthousiasme, ainsi que leurs organisations respectives, sans lesquelles cette publication n’aurait pas vu le jour.
Nos remerciements sont tgalement dos aux difftrentes personnes de la majorit6 des pays de I’OTAN qui ont foumi des
informations aux auteurs. Sans leur concours, cette AGARDographie aurait ttt moins complkte.