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Results 1 to 25 of 8973

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DESIGN OF SUPERCRITICAL SWEPT WINGSGARABEDIAN P; MCFADDEN G.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 3; PP. 289-291; BIBL. 11 REF.Article

SUPERCRITICAL REYNOLDS NUMBER SIMULATION FOR TWO-DIMENSIONAL FLOW OVER CIRCULAR CYLINDERS.SZECHENYI E.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 70; NO 3; PP. 529-542; BIBL. 9 REF.Article

PARAMETERS IN SUPERCRITICAL FLUID CHROMATOGRAPHY OF STYRENE OLIGOMERS.KLESPER E; HARTMANN W.1977; J. POLYM. SCI., POLYM. LETTERS ED.; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 707-712; BIBL. 4 REF.Article

ENTWICKLUNG UND WINDKANALERPROBUNG VON DREI UEBERKRITISCHEN TRAGFLUEGELPROFILEN FUER VERKEHRSFLUGZEUGE. = DEVELOPPEMENT ET EXPLORATION EN SOUFFLERIE DE TROIS PROFILS D'AILES SUPERCRITIQUES POUR AVIONS DE TRANSPORTSTANEWSKY E; ZIMMER H.1975; Z. FLUGWISSENSCH.; DTSCH.; DA. 1975; VOL. 23; NO 7-8; PP. 246-256; ABS. ANGL. FR.; BIBL. 14 REF.Article

REVIEW OF NASA SUPERCRITICAL AIRFOILS.WHITCOMB RT.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 8-18; BIBL. 21 REF.Conference Paper

ENTWICKLUNG VON NACHRECHNUNGSVERFAHREN FUER SUPERKRITISCHE FLUEGEL. = DEVELOPPEMENT DES METHODES DE CALCULS DE CONTROLE POUR LES AILES SUPERCRITIQUESKORNER H; KOSTER H; REDEKER G et al.1975; D.F.V.L.R.-NACHR.; DTSCH.; DA. 1975; NO 17; PP. 680-682Article

DETERIORATION OF HEAT TRANSFER TO SUPERCRITICAL HELIUM AT 2.5 ATMOSPHERES.GIARRATANO PJ; JONES MC.1975; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1975; VOL. 18; NO 5; PP. 649-653; BIBL. 9 REF.Article

CALCULATION OF TRANSONIC FLOW OVER SUPERCRITICAL AIRFOIL SECTIONS.ROSE WC; SEGINER A.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 8; PP. 514-519; BIBL. 16 REF.Article

THE THERMAL EFFICIENCY OF A PUMPED SUPERCRITICAL HELIUM REFRIGERATION SYSTEM OPERATING BELOW 6 K = LE RENDEMENT THERMIQUE D'UN SYSTEME DE REFRIGERATION A HELIUM SUPERCRITIQUE POMPE FONCTIONNANT EN DESSOUS DE 6 KDEAN JW.1974; CRYOGENICS; G.B.; DA. 1974; VOL. 14; NO 6; PP. 307-312; BIBL. 8 REF.Article

PROCEDIMENTO NUMERICO PER LA SOLUZIONE DEL PROBLEMA DIRETTO DEI PROFILI ALARI TRANSONICI SUPERCRITICI, CON METODO ODOGRAFICO.GEYMONAT G; GABUTTI B; NOCILLA S et al.1974; R.C. SEMINAR. MAT., TORINO; ITAL.; DA. 1974; VOL. 33; PP. 349-362; ABS. ANGL.Article

BREVET 2.221.186 (B) (7408577). A 13 MARS 1974. BROYEUR FONCTIONNANT A VITESSE SURCRITIQUE DE ROTATIONsdPatent

BREVET 2.290.486 (A1) (7533900). - 6 NOVEMBRE 1975. PERFECTIONNEMENTS A L'EXTRACTION HYDROGENANTE DU CHARBON.sdPatent

SUPERCRITICAL ACCRETION AND ITS POSSIBLE RELATION TO QUASARS AND RADIO SOURCESMEIER D.1982; SYMP.-INT. ASTRON. UNION; ISSN 0074-1809; NLD; DA. 1982; NO 97; PP. 263-264; BIBL. 5 REF.Conference Paper

ENTWURF UEBERKRISTISCHER PROFILE MIT HILFE DER RHEOELEKTRISCHEN ANALOGIE. = PROJET DE PROFILS SUPER-CRITIQUES A L'AIDE DE L'ANALOGIE RHEOELECTRIQUESOBIECZKY H.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 43; PP. 1-51; ABS. ANGL.; BIBL. 2 P.Article

PORTANCES INSTATIONNAIRES SUR UN CYLINDRE VIBRANT DANS UN ECOULEMENT SUPERCRITIQUE.SZECHENYI E; LOISEAU H.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 1; PP. 45-57; ABS. ANGL.; BIBL. 11 REF.Article

SUPERCRITICAL FLOW PAST SYMMETRICAL AIRFOILSKON MING LI; HOLT M.1982; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1982; VOL. 114; PP. 399-418; BIBL. 2 P.Article

A FINITE-DIFFERENCE METHOD FOR TRANSONIC AIRFOIL DESIGNSTEGER JL; KLINEBERG JM.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 628-635; BIBL. 9 REF.Serial Issue

TRANSIENT VOLTAGE RESPONSE OF A SUPERCONDUCTING STRIP TO A SUPERCRITICAL CURRENT PULSE = REPONSE DE TENSION TRANSITOIRE D'UNE BANDE SUPRACONDUCTRICE A IMPULSION DE COURANT SUPERCRITIQUEVAN ATTEKUM PMTM; WOUTERS MCHM; WOLTER J et al.1981; SOLID STATE COMMUN.; ISSN 0038-1098; USA; DA. 1981; VOL. 40; NO 11; PP. 1019-1020; BIBL. 6 REF.Article

THICK SUPERCRITICAL ACCRETION DISKS AND ACTIVE GALACTIC NUCLEIWIITA PJ.1982; COMMENT. ASTROPHYS.; ISSN 0146-2970; GBR; DA. 1982; VOL. 9; NO 6; PART. C; PP. 251-260; BIBL. 42 REF.Article

SUPERFICIAL AGE DEPENDENT BRANCHING PROCESSES WITH GENERATION DEPENDENCE.FEARN DH.1976; ANN. PROBAB.; U.S.A.; DA. 1976; VOL. 4; NO 1; PP. 27-37; BIBL. 7 REF.Article

CHEMICAL NATURE OF A SUPERCRITICAL-GAS EXTRACT OF COAL AT 350OC. = NATURE CHIMIQUE D'UN EXTRAIT DE CHARBON A 350OC PAR UN GAZ SUPERCRITIQUEBARTLE KD; MARTIN TG; WILLIAMS DF et al.1975; FUEL; G.B.; DA. 1975; VOL. 54; NO 4; PP. 226-235; BIBL. 61 REF.Article

THICK SUPERCRITICAL ACCRETION DISK AS A MODEL FOR SS433CALVANI M; NOBILI L.1981; VISTAS ASTRON.; ISSN 0083-6656; GBR; DA. 1981; VOL. 25; NO 1-2; PP. 173-176; BIBL. 3 REF.Conference Paper

RESEARCH ACTIVITIES ON COAL LIQUEFACTION IN THE UK = ACTIVITES DE RECHERCHE SUR LA LIQUEFACTION DU CHARBON EN GRANDE-BRETAGNEHARRISON JS.1976; AMER. CHEM. SOC., DIV. PETROLEUM CHEM., PREPR.; U.S.A.; DA. 1976; VOL. 21; NO 1; PP. 92-104Conference Paper

SUPERCRITICAL WING SECTIONS. II.BAUER F; GARABEDIAN P; KORN D et al.1975; LECTURE NOTES ECON. MATH. SYST.; GERM.; DA. 1975; VOL. 108; PP. (299P.); ISBN 354007029XSerial Issue

CONTRIBUTION A L'ETUDE DES DERIVATIONS DANS LES CANAUX DECOUVERTS.BOYER P.1974; ; S.L.; DA. 1974; PP. 1-153; (THESE DOCT. UNIV., MENTION MATH., SPEC. MEC.; PAUL SABATIER TOULOUSE)Thesis

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