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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

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

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

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

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

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

COMPUTATIONS OF UNSTEADY TRANSONIC CASCADE FLOWSNIXON D.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 790-792; BIBL. 3 REF.Article

COMPUTATIONAL FLUID DYNAMICS OF AIRFOILS AND WINGSGARABEDIAN P; MCFADDEN G.1982; TRANSONIC, SHOCK, AND MULTIDIMENSIONAL FLOWS-ADVANCES IN SCIENTIFIC COMPUTING. SYMPOSIUM ON TRANSONIC, SHOCK, AND MULTIDIMENSIONAL FLOWS/1981-05-13/MADISON WI; USA/GBR/FRA; NEW YORK; LONDON; PARIS: ACADEMIC PRESS; DA. 1982; PP. 1-16; BIBL. 16 REF.Conference Paper

TRANSONIC FLOW COMPUTATIONS USING GRID SYSTEMS WITH BLOCK STRUCTURELEE KD; RUBBERT PE.1981; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1981; NO 141; PP. 266-271; BIBL. 4 REF.Conference Paper

TRANSSONISCHE PROFILE IM EXPERIMENT = PROFILS TRANSSONIQUES A L'ESSAISTANEWSKY E.1980; D.F.V.L.R.-NACHR.; DEU; DA. 1980; NO 30; PP. 34-40Article

ON TRANSONIC FLOW IN A MOZZLEWEI TSENG.1979; J. MATH. ANAL. APPL.; USA; DA. 1979; VOL. 70; NO 1; PP. 85-100; BIBL. 21 REF.Article

BERECHNUNG DER TRANSSONISCHEN STROEMUNG DURCH EBENE TURBINENGITTER NACH DEM ZEIT-SCHRITT-VERFAHREN = CALCUL DES ECOULEMENTS TRANSSONIQUES DANS UNE GRILLE D'AUBES PLANES DE TURBINE PAR UNE METHODE DE DISCRETISATIONLEHTHAUS F.1978; V.D.I. FORSCH.-H.; DDR; DA. 1978; NO 586; PP. 5-24; BIBL. 1 P.Article

TRANSONIC AIRFOIL ANALYSIS AND DESIGN USING CARTESIAN COORDINATES.CARLSON LA.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 349-356; BIBL. 18 REF.Article

INVESTIGATION OF TRANSONIC LUDWIEG TUBES. I: STARTING PROCESS IN THE CASE OF AN UPSTREAM VALVEKAGE K; MATSUO K; KAWAGOE S et al.1983; BULLETIN OF THE JSME; ISSN 0021-3764; JPN; DA. 1983; VOL. 26; NO 215; PP. 778-784; BIBL. 5 REF.Article

SMALL DISTURBANCE TRANSONIC FLOW COMPUTATION, COMBINED WITH A FULL POTENTIAL CODELUNTZ A.1982; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 24/1982-02-17/TEL-AVIV, HAIFA; ISR; HAIFA: IMPR. AYALON OFFSET; DA. 1982; PP. 204-207; BIBL. 6 REF.Conference Paper

CHAMP NON-LINEAIRE LOINTAIN LORS DE L'ECOULEMENT TRANSONIQUE AUTOUR D'UN PROFIL NON-PORTANTSEVOST'YANOV GD.1982; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 6; PP. 171-173; BIBL. 5 REF.Article

APPLIED COMPUTATIONAL TRANSONIC AERODYNAMICS = METHODES DE CALCUL APPLIQUEES EN AERODYNAMIQUE TRANSSONIQUEHOLST TL; SLOOFF JW; YOSHIHARA H et al.1982; ; FRA; NEUILLY: A.G.A.R.D.; DA. 1982; AGARD/AG-266; 101 P.; 30 CM; BIBL. DISSEM.; ISBN 92-835-1431-9; AGARDOGRAPH; 266Report

INDICIAL APPROACH TO HARMONIC PERTURBATIONS IN TRANSONIC FLOWDAVIES DE; SALMOND DJ.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 1012-1014; BIBL. 2 REF.Article

LOW-FREQUENCY AND SMALL PERTURBATION EQUATION FOR TRANSONIC FLOW PAST WINGSCHAKRABARTTY SK; SUBRAMANIAN NR.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 9; PP. 1147-1149; BIBL. 6 REF.Article

THE NATIONAL TRANSONIC FACILITY: STATUS AND OPERATIONAL PLANNINGHOWELL RR.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 1-9; BIBL. 4 REF.Conference Paper

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