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Gasdynamische Effekte in transsonischen Strömungen durch Energiezu- und Abfuhr nach partiellem Phasenwechsel des FluidsSCHNERR, G. H.Zeitschrift für angewandte Mathematik und Mechanik. 1991, Vol 71, Num 5, pp T401-T408, issn 0044-2267Article

EFFETO DI SOLIDITA E INCIDENZA IN REGIME TRANSONICO SU SCHIERE DECELERATRICI FORTEMENTE CURVATE. = EFFETS DE LA SOLIDITE ET DE L'INCIDENCE DANS DES CASCADES TRANSSONIQUES A FORTE CAMBRURE EN DECELERATIONBISSANTI P; DI TOMMASO S; SCROFANI O et al.1976; TERMOTECNICA; ITAL.; DA. 1976; VOL. 30; NO 1; PP. 2-11; ABS. ANGL.; BIBL. 4 REF.Article

Ecoulement transsonique d'un jet gazeux à partir d'un récipient à parois planesKISELEV, O. M; KOZYREV, O. R.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1987, Num 6, pp 128-135, issn 0568-5281Article

Second-order-accurate spatial differencing for the transonic small-disturbance equationGOORJIAN, P. M; VAN BUSKIRK, R. D.AIAA journal. 1985, Vol 23, Num 11, pp 1693-1699, issn 0001-1452Article

Die Singularität in der Integralgleichung von Oswatitsch für transsonische Strömungen = Singularity in Oswatitsh integral equation for transonic flowsZIEREP, J.Zeitschrift für angewandte Mathematik und Mechanik. 1994, Vol 74, Num 5, pp T384-T386, issn 0044-2267Article

Über das einparametrige Verfahren zur Berechnung der transsonischen StrömungCIALKOWSKI, M. J.Zeitschrift für angewandte Mathematik und Mechanik. 1991, Vol 71, Num 5, pp T434-T437, issn 0044-2267Article

Contribution au calcul de l'écoulement transsonique dans les turbomachines par la méthode potentielle = Contribution to the computation of the transonic flows in turbomachinery using the potential methodLan, Qiang; Chauvin, Jacques.1989, 139 p.Thesis

Approximations d'ordre élevé dans la décomposition transsonique de la solution des équations de ChaplyginCHERNOV, I. A.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 4, pp 169-171, issn 0568-5281Article

UN IMPIANTO SPERIMENTALE PER RICERCHE FLUODINAMICHE IN CAMPO TRANSONICO = UN DISPOSITIF EXPERIMENTAL DE RECHERCHE EN DYNAMIQUE DES FLUIDES DANS LE DOMAINE TRANSSONIQUEACTON O; PITTALUGA F.1982; TERMOTECNICA; ISSN 0040-3725; ITA; DA. 1982; VOL. 36; NO 6; PP. 63-70; ABS. ENG; BIBL. 16 REF.Article

TRANSONIC SHOCK-FREE AEROFOIL DESIGN BY AN ANALYTIC HODOGRAPH METHOD.BOERSTOEL JW; HUIZING GH.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 730-736; BIBL. 11 REF.Article

A SURVEY OF TRANSONIC AERODYNAMICS.WU JM; MOULDEN TH.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 326; PP. 1-37; BIBL. 9 P. 1/2Conference Paper

COMPARISON OF PRESSURE AND LDV VELOCITY MEASUREMENTS WITH PREDICTIONS IN TRANSONIC FLOW.FLACK RD; THOMPSON HD.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 1; PP. 53-59; BIBL. 24 REF.Article

COMPUTATION OF TRANSONIC FLOW ABOUT LIFTING WING-CYLINDER COMBINATIONS.KLUNKER EB; NEWMAN PA.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 254-256; BIBL. 16 REF.Article

APPROXIMATE SHOCK-FREE TRANSONIC SOLUTION OF LIFTING AIRFOILS.SUNIL KUMAR CHAKRABARTTY.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 1094-1097; BIBL. 10 REF.Article

COMMANDE EN TEMPS REEL DU NOMBRE DE MACH DANS UNE SOUFFLERIE TRANSSONIQUE A RAFALES.GOBERT JL.1975; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1975; PP. 1-66; ABS. ANGL.; BIBL. 20 REF.; (THESE DOCT. 3E CYCLE; PARIS VI; 1975)Thesis

AN EXACT SOLUTION TO THE TRANSONIC EQUATION.BIBLARZ O.1975; ISRAEL J. TECHNOL.; ISRAEL; DA. 1975; VOL. 13; NO 4; PP. 229-236; BIBL. 6 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

MESH GENERATION STRATEGIES FOR CFD ON COMPLEX CONFIGURATIONSLEICHER S; FRITZ W; GRASHOF J et al.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 328-334; BIBL. 17 REF.Conference Paper

FLOW IN TRANSONIC COMPRESSORSKERREBROCK JL.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 1; PP. 4-19; BIBL. 50 REF.Article

LOAD DISTRIBUTION ON A CLOSE-COUPLED WING CANARD AT TRANSONIC SPEEDS.GLOSS BB; WASHBURN KE.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 4; PP. 234-239; BIBL. 15 REF.Article

BESTIMMUNG SYMMETRISCHER TRANSSONISCHER PROFILSTROEMUNGEN MITTELS LEGENDRE-TRANSFORMATION. = DETERMINATION DES ECOULEMENTS AUTOUR DES PROFILS SYMETRIQUES TRANSSONIQUES AU MOYEN DE LA TRANSFORMATION DE LEGENDRESTREHMEL K.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 11; PP. 671-679; ABS. ANGL. RUSSE; BIBL. 12 REF.Article

SUPPRESSION OF BACKGROUND NOISE IN A TRANSONIC WIND-TUNNEL TEST SECTION. = SUPPRESSION DU BRUIT DE FOND DANS UNE SECTION D'ESSAI DE SOUFFLERIE TRANSSONIQUESCHUTZENHOFER LA; HOWARD PW.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 11; PP. 1467-1471; BIBL. 16 REF.Article

CALCULATION OF TRANSONIC FLOW AROUND AXISYMMETRIC INLETS.ARLINGER BG.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1614-1621; BIBL. 12 REF.Article

BLADE-TO-BLADE FLOW EFFECTS ON MEAN FLOW IN TRANSONIC COMPRESSORSSEHRA AK; KERREBROCK JL.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 4; PP. 476-483; BIBL. 15 REF.Article

COMPARISON OF TESTING TECHNIQUES FOR ISOLATED AXISYMMETRIC EXHAUST NOZZLES IN TRANSONIC FLOW.LAUGHREY JA.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1292; PP. 1-11; BIBL. 9 REF.Conference Paper

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