000 04518nam a22004695i 4500
001 978-3-540-38392-5
003 DE-He213
005 20190213151618.0
007 cr nn 008mamaa
008 121227s1973 gw | s |||| 0|eng d
020 _a9783540383925
_9978-3-540-38392-5
024 7 _a10.1007/BFb0112668
_2doi
050 4 _aQC120-168.85
050 4 _aQA808.2
072 7 _aPHD
_2bicssc
072 7 _aSCI041000
_2bisacsh
072 7 _aPHD
_2thema
082 0 4 _a531
_223
245 1 0 _aProceedings of the Third International Conference on Numerical Methods in Fluid Mechanics
_h[electronic resource] :
_bVol. II Problems of Fluid Mechanics /
_cedited by Henri Cabannes, Roger Temam.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c1973.
300 _aVII, 279 p. 77 illus.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aLecture Notes in Physics,
_x0075-8450 ;
_v19
505 0 _aA numerical method for highly accelerated laminar boundary-layer flows -- Relaxation methods for transonic flow about wing-cylinder combinations and lifting swept wings -- Calcul D’un Ecoulement Viscoelastique Dans une Cavite Carree -- Oscillations Libres d’un Bassin en Rotation -- Numerical approach for investigating some transsonic flows -- The computation of three-dimensional viscous internal flows -- Inviscid reattachment of a separated shear layer -- Time dependent calculations for transonic flow -- Two calculation procedures for steady, three-dimensional flows with recirculation -- Numerical solutions of the supersonic, laminar flow over a two-dimensional compression corner -- Laminar boundary layers with assigned wall shear -- Application de la Methode Hodographique au Traitement des Ecoulements Transsoniques Avec Onde de Choc -- Finite difference treatment of strong shock over a sharp leading edge with navier-stokes equations -- A vortex method for the study of rapid flow -- Numerical studies of the heat conduction equation with highly anisotropic tensor conductivity -- Turbulence transitions in convective flow -- The numerical solution of the vorticity transport equation -- Reflexions D’ondes de Choc Sur L’axe en Ecoulement Permanent de Revolution -- Computational problems in three and four dimensional boundary layer theory -- A direct method for computing the steady flow at mach number one past a given wing airfoil -- The structure of a reflecting oblique shock wave -- Calculation of separated flows at subsonic and transonic speeds -- Numerical solutions of blast wave propagation problems -- Stratified flow over a vertical barrier -- Developement de la Methode Des Singularites a Repartition Discretisee Pour L’Etude Des Ecoulements Incompressibles et Compressibles -- The numerical solution of convective heat transfer in the space shuttle base region by Telenin’s method -- A relaxation method for calculating transonic flows with detached bow shocks -- Transient three-dimensional fluid flow in the vicinity of large structures -- Flow patterns around heart valves -- Calcul de L’ecoulement D’un Fluide Visqueux Compressible Autour D’un Obstacle de Forme Parabolique -- Solutions Numeriques des Equations de Navier-Stokes Pour les Ecoulements en Couches Visqueuses -- Numerical simulation of small-scale thermal convection in the atmosphere -- Some comparisons between mixing-length and turbulent energy equation models of flow above a change in surface roughness -- Numerical solution of the unsteady navier-stokes equations in curvilinear coordinates: The hypersonic blunt body merged layer problem -- Probleme de Mecanique des Fluides, non Lineaires, Stationnaires en Meteorologie.
650 0 _aMechanics.
650 1 4 _aClassical Mechanics.
_0http://scigraph.springernature.com/things/product-market-codes/P21018
700 1 _aCabannes, Henri.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
700 1 _aTemam, Roger.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783540061717
776 0 8 _iPrinted edition:
_z9783662212028
830 0 _aLecture Notes in Physics,
_x0075-8450 ;
_v19
856 4 0 _uhttps://doi.org/10.1007/BFb0112668
912 _aZDB-2-PHA
912 _aZDB-2-LNP
912 _aZDB-2-BAE
999 _c11273
_d11273