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Results 1 to 25 of 1972

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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

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

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

FINITE DIFFERENCE COMPUTATION OF THE AERODYNAMIC INTERFERENCE OF WING-PYLON-STORE COMBINATIONS AT TRANSONIC SPEEDSPAN NQ; WANG WF; XU SJ et al.1983; COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING; ISSN 0045-7825; NLD; DA. 1983; VOL. 37; NO 1; PP. 1-13; BIBL. 3 REF.Article

A TRANSONIC QUASI-3D ANALYSIS FOR GAS TURBINE ENGINES INCLUDING SPLIT-FLOW CAPABILITY FOR TURBOFANSHABASHI WG; YOUNGSON GG.1983; INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS; ISSN 0271-2091; GBR; DA. 1983; VOL. 3; NO 1; PP. 1-21; BIBL. 20 REF.Article

ARTIFICIAL EVOLUTION TECHNIQUES FOR TRANSONIC FLOWSESSERS JA.1982; NUMERICAL METHODS FOR FLOWS IN TURBOMACHINERY BLADINGS. COURSE/1982/RHODE-SAINT-GENESE; BEL; RHODE-SAINT-GENESE: VON KARMAN INSTITUTE FOR FLUID DYNAMICS; DA. 1982; VOL. 1; PP. 1-99; H.T. 32; BIBL. 47 REF.Conference Paper

TRANSONIC FLOW COMPUTATIONS IN CASCADES USING FINITE ELEMENT METHODAKAY HU; ECER A.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 4; PP. 657-664; BIBL. 9 REF.Article

A REVIEW OF METHODS FOR PREDICTING VISCOUS EFFECTS ON AEROFOILS AND WINGS AT TRANSONIC SPEEDSLOCK RC.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 2.1-2.32; BIBL. 62 REF.Article

CALCULATION OF UNSTEADY TRANSONIC FLOW OVER AN AIRFOILCHYU WJ; DAVIS SS; CHANG KS et al.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 6; PP. 684-690; BIBL. 18 REF.Article

IMPROVED VERSION OF LTRAN2 FOR UNSTEADY TRANSONIC FLOW COMPUTATIONSHOUWINK R; VAN DER VOOREN J.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 1008-1010; BIBL. 4 REF.Article

INTERACTION AERODYNAMIQUE ENTRE UN CANARD PROCHE ET UNE AILE EN FLECHE EN ECOULEMENT TRANSSONIQUEBROCARD Y; SCHMITT V.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 23 P.; ABS. ENG; BIBL. 15 REF.Conference Paper

THE PRESENT STATE IN THE AXIAL-FLOW TRANSONIC COMPRESSOR DESIGNCELIKOVSKY K.1979; CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 1; PP. 189-199; BIBL. 8 REF.Conference Paper

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