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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

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

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

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

Non-equilibrium condensation of water vapor in sonic nozzleHONGBING DING; CHAO WANG; CHAO CHEN et al.Applied thermal engineering. 2014, Vol 71, Num 1, pp 324-334, issn 1359-4311, 11 p.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

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

A FAST PSEUDO-TIME INTEGRATION SCHEME FOR THE STEADY TRANSONIC FLOW PROBLEMYURTSEVEN HO; KARACA C; ECER A et al.1982; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1982; VOL. 34; NO 1-3; PP. 787-800; BIBL. 4 REF.Conference Paper

MODIFICATION OF WING SECTIONS TO OPTIMIZE TRANSONIC PERFORMANCELUNTZ A; BARNETT Y; DAREL I et al.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 2/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 1-4; BIBL. 2 REF.Conference Paper

LIFT CORRECTIONS TO TRANSONIC EQUIVALENCE RULE; EXAMPLES.CHENG HK.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 366-373; BIBL. 22 REF.Article

APPLICATION DE LA METHODE D'ETABLISSEMENT A LA RESOLUTION NUMERIQUE DU PROBLEME DIRECT D'UNE CASCADE PLANE DE PROFILSSOKOLOVSKIJ GA; GNESIN VI; NAZARENKO RA et al.1976; PROBL. MASHINOSTR., U.S.S.R.; S.S.S.R.; DA. 1976; NO 3; PP. 78-85; 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

Unsteady radial transport in a transonic compressor stageKOTIDIS, P. A; EPSTEIN, A. H.Journal of mechanical design (1990). 1991, Vol 113, Num 2, pp 207-218, issn 1050-0472Conference Paper

An investigation of the flow characteristics of transonic nozzle bladesVENEDIKTOV, V. D; GRANOVSKIJ, A. V; KOLESOV, A. N et al.Teploenergetika (Moskva, 1954). 1989, Num 8, pp 53-56, issn 0040-3636, 4 p.Article

Steady and unsteady transonic pressure distributions on NACA 0012TRIEBSTEIN, H.Journal of aircraft. 1986, Vol 23, Num 3, pp 213-219, issn 0021-8669Article

A new fast solver procedure applied to the BGK computer program for transonic flow past on airfoilYAU SHU WONG; JONES, D. J.Canadian aeronautics and space journal. 1985, Vol 31, Num 2, pp 159-169, issn 0008-2821Article

Transonic time responses of the MBB A-3 supercritical airfoil including active controlsBATINA, J. T; YANG, T. Y.Journal of aircraft. 1985, Vol 22, Num 5, pp 393-400, issn 0021-8669Article

A multi-grid method for transonic wing analysis and designPRADEEP RAJ.Journal of aircraft. 1984, Vol 21, Num 2, pp 143-150, issn 0021-8669Article

Engine power simulation for transonic flow-through nacellesCHIN, W. C.AIAA journal. 1983, Vol 21, Num 10, pp 1471-1472, issn 0001-1452Article

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