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ARE BIPOLAR NEBULAE BICONICAL.ICKE V.1981; ASTROPHYS. J.; ISSN 0004-637X; USA; DA. 1981; VOL. 247; NO 1; PART. 1; PP. 152-157; BIBL. 38 REF.Article

A SOLUTION FOR CONICALLY CAMBERED DELTA WINGS IN SUPERSONIC FLOW.MATEESCU D.1975; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1975; VOL. 20; NO 2; PP. 189-216; BIBL. 7 REF.Article

SUPERSONIC MOTION AROUND A POROUS CONE WITH FLUID INJECTION.CARAFOLI E; BERBENTE C.1976; MECH. RES. COMMUNIC.; G.B.; DA. 1976; VOL. 3; NO 3; PP. 185-190; BIBL. 5 REF.Article

AN EXPERIMENTAL INVESTIGATION OF THREE-DIMENSIONAL SHOCK WAVES INDUCED BY GAS INJECTION THROUGH TWO ORIFICES INTO SUPERSONIC CONICAL FLOW.YAMANAKA T; KAMIMURA H.1975; BULL. J.S.M.E.; JAP.; DA. 1975; VOL. 18; NO 121; PP. 689-699; BIBL. 15 REF.Article

THE SUPERSONIC FLOW AROUND A SHARP-NOSE ELLIPTIC CONE AT THE ANGLE OF ATTACK.VETLUTSKII VN; GANIMEDOV VL.1974; ARCH. MECH.; POLAND; DA. 1974; VOL. 26; NO 4; PP. 647-652; ABS. POL. RUSSE; BIBL. 7 REF.Article

SOLUTION OF CONICAL-SUBSONIC FLOWS BY THE METHOD OF SERIES TRUNCATION.NADIR S.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ.; DA. 1975; VOL. 26; NO 1; PP. 1-11; ABS. FR.; BIBL. 6 REF.Article

CONICAL POTENTIAL FLOW ABOUT BODIES OF REVOLUTION.MILOH T.1976; QUART. J. MECH. APPL. MATH.; G.B.; DA. 1976; VOL. 29; NO 1; PP. 35-60; BIBL. 30 REF.Article

AGREEMENT OF HIGH CONICAL FLOW THEORY WITH EXPERIMENTAL RESULTS FOR SUPERSONIC FLOWNASTASE A.1980; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T199-T201; BIBL. 8 REF.Article

SOME PROBLEMS OF THE THEORY OF CONICAL GAS FLOWS.TESHUKOV VM.1976; ARCH. MECH.; POLAND; DA. 1976; VOL. 28; NO 5-6; PP. 781-786; ABS. POL. ANGL.; BIBL. 4 REF.Article

ETUDE DES CHAMPS DE VITESSE ET DES PRESSIONS STATIQUES DES ECOULEMENTS A UNE PHASE SORTANT DE CANAUX CONIQUESAZIZOV BM; PONIKAROV II; BAGAUTDINOV NI et al.1979; Z. PRIKL. HIM.; ISSN 0044-4618; SUN; DA. 1979; VOL. 52; NO 7; PP. 1651-1652; BIBL. 7 REF.Article

A HIGHER-ORDER PANEL METHOD FOR THE COMPUTATION OF THE FLOW ABOUT SLENDER DELTA WINGS WITH LEADING-EDGE VORTEX SEPARATIONHOEIJMAKERS HWM; VAATSTRA W.1982; CONFERENCE ON NUMERICAL METHODS IN FLUID MECHANICS. 4/1981/PARIS; DEU; BRAUNSCHWEIG; WIESBADEN: F. VIEWEG; DA. 1982; PP. 137-149; BIBL. 19 REF.Conference Paper

MISE EN FORME DU PROBLEME MIXTE - DANS LE CAS D'UN SYSTEME NON STATIONNAIRE D'EQUATIONS DIFFERENTIELLES - UTILISE POUR CALCULER NUMERIQUEMENT DES ECOULEMENTS DE GAZ DE FORME CONIQUE, STATIONNAIRES ET SUPERSONIQUESBLOKHIN AM.1979; CHISLENN. METODY MEKH. SPLOSHN. SREDY; SUN; DA. 1979; VOL. 10; NO 1; PP. 31-44; BIBL. 9 REF.Article

ANTISYMMETRIC PROBLEMS IN SHOCK DIFFRACTION THEORYGUNZBURGER MD; YANG VK.1973; Z. ANGEW MATH. PHYS.; SCHWEIZ; DA. 1973; VOL. 24; NO 1; PP. 83-104; ABS. FR.; BIBL. 15 REF.Serial Issue

Vectorized schemes for conical potential flow using the artificial density methodBRADLEY, P. F; DWOYER, D. L; SOUTH, J. C. JR et al.AIAA journal. 1986, Vol 24, Num 1, pp 13-20, issn 0001-1452Article

TEMPERATURE D'UN CONE RAYONNANT DANS UN ECOULEMENT SUPERSONIQUE DE GAZ TRANSPARENTIVANOV VV; DUNIN IL.1972; TEPLOFIZ. VYS. TEMPER.; S.S.S.R.; DA. 1972; VOL. 10; NO 5; PP. 1124-1126; BIBL. 7 REF.Serial Issue

A PERTURBATION METHOD FOR CONICAL MOTIONS CONSIDERING THE ENTROPY-LAYER EFFECTSBERBENTE C.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 6; PP. 1205-1222; BIBL. 10 REF.Serial Issue

THE SPLIT-COEFFICIENT MATRIX METHOD FOR HYPERBOLIE SYSTEMS OF GAS DYNAMIC EQUATIONSCHAKRAVARTHY SR; ANDERSON DA; SALAS MD et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 20 P.; BIBL. 11 REF.Conference Paper

POTENTIAL FLOW NEAR CONICAL STAGNATION POINTSBAKKER PG; BANNINK WJ; REYN JW et al.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 105; PP. 239-260; BIBL. 16 REF.Article

FLOW PATTERNS NEAR A CONICAL SONIC LINESALAS MD.1980; A.I.A.A. J., NEW YORK; USA; DA. 1980; VOL. 18; NO 3; PP. 227-234; BIBL. 18 REF.Article

A NUMERICAL METHOD FOR SUPERSONIC CONICAL FLOW WITHOUT AXIAL SYMMETRY.SUGIYAMA H.1977; BULL. J.S.M.E.; JAP.; DA. 1977; VOL. 20; NO 144; PP. 711-717; BIBL. 8 REF.Article

DETERMINATION DES ONDES DE COMBUSTION DANS UN ECOULEMENT CONIQUE SUPERSONIQUECARAFOLI E; DUMITRESCU H.1973; STUD. CERC. MEC. APL.; ROMAN.; DA. 1973; VOL. 32; NO 2; PP. 259-275; BIBL. 6 REF.Serial Issue

Rapid conical flows of viscoelastic solutionsOLIVER, D. R.Journal of non-newtonian fluid mechanics. 1984, Vol 16, Num 3, pp 267-277, issn 0377-0257Article

Cylindrical and conical flow regimes of three-dimensional shock/boundary-layer interactionsSETTLES, G. S; HSUEH-YING TENG.AIAA journal. 1984, Vol 22, Num 2, pp 194-200, issn 0001-1452Article

Caractéristiques géométriques du décollement de la couche limite turbulente lors de l'interaction avec une discontinuité linéaire de condensation dans les écoulements coniquesZUBIN, M. A; OSTAPENKO, N. A.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1983, Num 6, pp 43-51, issn 0568-5281Article

Emploi du diviseur conique pour le contrôle de qualité détergents synthétiquesKRAL-OSIKINA, G. A; PERLOVA, K. R; KUDAEVA, V. S et al.Maslo-žirovaâ promyšlennost'. 1984, Num 7, pp 19-21, issn 0025-4649Article

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