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

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

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

COMPUTER SIMULATION OF TRANSONIC FLOW PAST AIRFOILS WITH BOUNDARY LAYER CORRECTION. = SIMULATION SUR CALCULATRICE ELECTRONIQUE DE L'ECOULEMENT TRANSSONIQUE AUTOUR DES PROFILS AERODYNAMIQUES AVEC CORRECTION DE COUCHE LIMITEBAUER F; KORN D.1975; IN: COMPUT. FLUID DYN. CONF. 2. PROC.; HARTFORD, CONN.; 1975; S.L.; AIAA; DA. 1975; PP. 184-204; BIBL. 15 REF.Conference Paper

THE ROLE OF THE NAE 5X5 FOOT WIND TUNNEL IN THE DEVELOPMENT OF MODERN AIRFOIL SECTION.OHMAN LH.1975; IN: ANGLO-AM. AERONAUT. CONF. 14. TECH. PAP.; LOS ANGELES, CALIF.; 1975; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1975; VOL. 959; PP. 1-15; BIBL. 1 P. 1/2Conference Paper

EIN INSTATIONAERES VERHALTEN TRANSSONISCHER STROEMUNGEN. = UN COMPORTEMENT INSTATIONNAIRE DES ECOULEMENTS TRANSSONIQUESMEIER GEA.1974; MITT. MAX-PLANCK-INST. STROEMUNGSFORSCH. AERODYN. VERSUCHSANST.; DTSCH.; DA. 1974; NO 59; PP. (138P.); BIBL. 5 P.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

REPRESENTATION ASYMPTOTIQUE SUR LE PLAN D'UN HODOGRAPHE DES SOLUTIONS DE PROBLEMES D'ECOULEMENT TRANSSONIQUE SUR DES PROFILSDOBROVOL'SKAYA ZN.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 84-88; BIBL. 9 REF.Article

TRANSONIC EQUIVALENCE RULE: A NONLINEAR PROBLEM INVOLVING LIFT.CHENG HK; HAFEZ MM.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 1; PP. 161-187; BIBL. 1 P. 1/2Article

TRANSONIC FLOW OVER AN AEROFOIL WITH SPOILER.KANIA W.1975; ROZPR. INZYN.; POLSKA; DA. 1975; VOL. 23; NO 4; PP. 587-596; ABS. POL. RUSSE; BIBL. 11 REF.Article

TRAGENDE SCHNABELPROFILE IN STOSSFREIER SCHALLANSTROEMUNG. = PROFILS PORTANTS A BORDS D'ATTAQUE AIGUS DANS UN ECOULEMENT INCIDENT TRANSSONIQUE SANS CHOCSOBIECZKY H.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 6; PP. 819-830; ABS. ANGL.; BIBL. 4 REF.Article