Contribution à l'étude de l'écoulement dans un tube à choc PDF Download
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Author: G. Devanlay
Publisher:
ISBN:
Category :
Languages : fr
Pages : 83
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Author: G. Devanlay
Publisher:
ISBN:
Category :
Languages : fr
Pages : 83
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Author: Joël Doffin
Publisher:
ISBN:
Category :
Languages : fr
Pages : 428
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Author: Miguel Moron
Publisher:
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Category :
Languages : fr
Pages : 200
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Author:
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ISBN:
Category :
Languages : fr
Pages :
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Category : Aeronautics
Languages : en
Pages : 830
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: FADWA.. ALHAMWI/HEIR-BECK
Publisher:
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Category :
Languages : fr
Pages :
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L'ETUDE PORTE SUR L'ANALYSE DES ECOULEMENTS INSTATIONNAIRES EN TUBE A ONDE DE CHOC, AVEC PRISE EN COMPTE DES PHENOMENES LIES A LA VISCOSITE DU FLUIDE, A PARTIR D'UNE INTEGRATION DIRECTE DES EQUATIONS DE NAVIER-STOKES AVEC UN MODELE DE TURBULENCE SOIT EN (K) SOIT EN LONGUEUR DE MELANGE. AU COURS DE CETTE ETUDE IL A ETE, D'UNE PART, TRAITE DE MANIERE SEPAREE LA PARTIE ONDE DE DETENTE ET LA PARTIE ONDE DE CHOC (COAURBURE ET STRUCTURE), ET D'AUTRE PART A ETE EFFECTUE UN TRAITEMENT GLOBAL DE L'ECOULEMENT. LES RESULTATS DE CALCUL ONT ETE COMPARES AVEC CEUX OBTENUS PAR D'AUTRES VOIES THEORIQUES AINSI QU'AVEC DES DONNEES EXPERIMENTALES. LA RESOLUTION DES EQUATIONS DE NAVIER-STOKES EST EFFECTUEE PAR UNE METHODE AUX DIFFERENCES FINIES UTILISANT LE SCHEMMA EXPLICITE A DEUX PAS PREDICTEUR-CORRECTEUR DE MAC-CORMACK
Author: Malek Bouhadef
Publisher:
ISBN:
Category :
Languages : fr
Pages : 196
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Category : Aeronautics
Languages : en
Pages : 1166
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Author: Wilbur C. Nelson
Publisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
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The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
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Category :
Languages : fr
Pages : 0
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