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SUR LES PROFILS AERODYNAMIQUES.COUCHET G; LAPORTE R.1975; J. MEC.; FR.; DA. 1975; VOL. 14; NO 3; PP. 523-530; ABS. ANGL.; BIBL. 7 REF.Article

SUR LA CONSTRUCTION DE PROFILS AERODYNAMIQUES VOISINS D'UN PROFIL DONNELAPORTE R.1978; J. MEC.; FRA; DA. 1978; VOL. 17; NO 2; PP. 207-229; ABS. ENG; BIBL. 20 REF.Article

DISCRETE TONES OF ISOLATED AIRFOILS.TAM CKW.1974; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1974; VOL. 55; NO 6; PP. 1173-1177; BIBL. 11 REF.Article

CAMBERED VALVE LEAFLETS THAT MAXIMIZE INITIAL RATE OF CLOSURETUCK EO; HELFGOTT A; YEUNG RW et al.1982; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1982; VOL. 121; PP. 517-529; BIBL. 5 REF.Article

COMMENT ON "POTENTIAL FLOW ANALYSIS OF MULTIELEMENT AIRFOILS USING CONFORMAL MAPPINGLAURA PAA.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 6; PP. 830; BIBL. 13 REF.Article

UNSTEADY AERODYNAMICS OF AN AEROFOIL AT HIGH ANGLE OF INCIDENCE PERFORMING VARIOUS LINEAR OSCILLATIONS IN A UNIFORM STREAMMARESCA CA; FAVIER DJ; REBONT JM et al.1981; J. AM. HELICOPTER SOC.; ISSN 0002-8711; USA; DA. 1981; VOL. 26; NO 2; PP. 40-45; BIBL. 8 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

ETUDE DE L'EMISSION SONORE D'UN PROFIL ISOLE PLACE DANS LE CHAMP HYDRODYNAMIQUE INDUIT PAR UNE ZONE DE MELANGE.ARBEY H; SUNYACH M; COMTE BELLOT G et al.1975; C.R. ACAD. SCI., B; FR.; DA. 1975; VOL. 281; NO 20; PP. 489-492; ABS. ANGL.; BIBL. 4 REF.Article

ETUDE DU BUFFETING DES PROFILS AUX INCIDENCES CRITIQUES EN REGIME INCOMPRESSIBLE.TENSI J.1975; AO-CNRS-10939; FR.; DA. 1975; PP. (79P.); H.T. 115; BIBL. 3 P. 1/2; (THESE DOCT. ING.; POITIERS)Thesis

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

THEORIE ASYMPTOTIQUE D'UN PROFIL D'AILE D'ALLONGEMENT MOYENEFREMOV II.1974; GIDROMEKHANIKA, U.S.S.R.; S.S.S.R.; DA. 1974; NO 29; PP. 10-13; BIBL. 6 REF.Article

HIGHER ORDER SIMILARITY SOLUTIONS FOR HYPERSONIC AEROFOILS.HUI WH; HEMDAN HT.sdIN: SYMMETRY, SIMILARITY GROUP THEOR. METHODS MECH. PROC. SYMP.; CALGARY; 1974; S.L.; DA. S.D.; PP. 403-417; BIBL. 7 REF.Conference Paper

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

ETUDE THEORIQUE ET EXPERIMENTALE DES CARACTERISTIQUES AERODYNAMIQUES DE CORPS TRIDIMENSIONNELSGUSAROV AA; DVORETSKIJ VM; IVANOV M YA et al.1979; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1979; NO 3; PP. 97-102; BIBL. 11 REF.Article

METHODE DE CALCUL DES COEFFICIENTS AERODYNAMIQUES DE CERTAINS CORPS VOLUMINEUX DE SECTION TRANSVERSE QUELCONQUESKIBA GG; FEDOTOV BN.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 92-98; BIBL. 2 REF.Article

PROBLEME NON-LINEAIRE DU MOUVEMENT D'UN PROFIL PRES D'UNE PAROI ONDULEESHUMSKIJ GM.1977; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1977; NO 2; PP. 79-84; BIBL. 9 REF.Article

ETUDE DE L'EMISSION SONORE D'UN PROFIL ISOLE PLACE A DIFFERENTES INCIDENCES.ARBEY H; SUNYACH M; COMTE BELLOT G et al.1975; C.R. ACAD. SCI., B; FR.; DA. 1975; VOL. 281; NO 15; PP. 285-288; ABS. ANGL.; BIBL. 5 REF.Article

GEARED-ELEVATOR FLUTTER STUDY.RUHLIN CL; DOGGETT RV JR; GREGORY RA et al.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 598-607; BIBL. 5 REF.Conference Paper

THE FLOW ABOUT THE TRAILING EDGE OF A SUPERSONIC OSCILLATING AEROFOIL. = ECOULEMENT AUTOUR DU BORD DE FUITE D'UN PROFIL AERODYNAMIQUE OSCILLANT SUPERSONIQUEDANIELS PG.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 3; PP. 541-557; BIBL. 25 REF.Article

MOUVEMENT D'UN PROFIL D'AILE SEMI-ELLIPTIQUE AU VOISINAGE D'UN ECRANZINCHUK PI; YUKHIMENKO AI.1974; GIDROMEKHANIKA, U.S.S.R.; S.S.S.R.; DA. 1974; NO 28; PP. 61-69; BIBL. 8 REF.Article

COMPUTATIONAL MODEL FOR LOW-SPEED FLOWS PAST AIRFOILS WITH SPOILERSPFEIFFER NJ; ZUMWALT GW.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 3; PP. 376-382; BIBL. 20 REF.Article

DESIGN OF ADVANCED TECHNOLOGY TRANSONIC AIRFOILS AND WINGSSOBIECZKY H.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 13 P.; BIBL. 32 REF.Conference Paper

CALCUL DE L'ECOULEMENT AUTOUR D'UN PROFIL POUR UNE CHALEUR MASSIQUE VARIABLESIDOROV OP.1980; IZV. VYSS. UCEBN. ZAVED., AVIAC. TEH.; ISSN 0579-2975; SUN; DA. 1980; NO 2; PP. 77-82; BIBL. 2 REF.Article

AN IMPROVED IN THE TREATMENT OF SEPARATION IN GENERAL CASCADES BY POTENTIAL FLOW METHODSKADHIM SJ; RAILLY JW.1980; PROC.-INST. MECH. ENG.; ISSN 0020-3483; GBR; DA. 1980-09; VOL. 194; PP. 195-201; BIBL. 6 REF.Article

UNSTEADY AERODYNAMIC MODELING FOR ARBITRARY MOTIONS.EDWARDS JW.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 593-595; BIBL. 6 REF.Article

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