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AERODYNAMIC INTERFERENCE EFFECTS ON OSCILLATING AIRFOILS WITH CONTROLS IN VENTILATED WIND TUNNELSFROMME JA; GOLBERG MA.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 4; PP. 417-426; BIBL. 36 REF.Article

CONFORMAL REPRESENTATION OF ARBITRARY MULTICONNECTED AIRFOIL SECTIONS.PROSNAK WJ.1977; BULL. ACAD. POLON. SCI., SCI. TECH.; POLOGNE; DA. 1977; VOL. 25; NO 7; PP. 25-36; ABS. RUSSE; BIBL. 11 REF.Article

UNSTEADY WAKE MEASUREMENTS OF AIRFOILS AND CASCADES.SATYANARAYANA B.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 5; PP. 613-618; BIBL. 15 REF.Article

MOMENTENBEIWERT DER EINZEL-ODER GITTERPROFILE. = COEFFICIENT DE MOMENT POUR LE PROFIL ISOLE OU POUR LA CASCADE DE PROFILSZIDARU G.1977; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1977; VOL. 22; NO 5; PP. 761-772; BIBL. 9 REF.Article

INSTANTANEOUS TURBULENCE PROFILES IN THE WAKE OF AN OSCILLATING AIRFOILDE RUYCK J; HIRSCH C.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 641-642; BIBL. 5 REF.Article

ANALYSIS OF TRANSONIC FLOW ABOUT HARMONICALLY OSCILLATING AIRFOILS AND WINGSWEATHERILL WH; EHLERS FE.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 8 P.; BIBL. 12 REF.Conference Paper

FLOW SIMULATION BY DISCRETE VORTEX METHODOSHIMA K; OSHIMA Y.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 94-106; BIBL. 2 P.Conference Paper

PREDICTION OF BOUNDARY LAYER CHARACTERISTICS OF AN OSCILLATING AIRFOILCEBECI T; CARR LW.1981; UNSTEADY TURBULENT SHEAR FLOWS. SYMPOSIUM ON UNSTEADY TURBULENT SHEAR FLOWS/1981/TOULOUSE; DEU/USA; BERLIN; NEW YORK: SPRINGER; DA. 1981; PP. 145-158; BIBL. 13 REF.Conference Paper

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

VISCOUS-INVISCID INTERACTION ON OSCILLATING AIRFOILS IN SUBSONIC FLOWMCCROSKEY WJ; PUCCI SL.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 16 P.; BIBL. 11 REF.Conference Paper

RIGOROUS SOLUTION OF COMPRESSIBLE POTENTIAL FLOW PAST TWO-DIMENSIONAL CASCADES OF AIRFOILS: ESPECIALLY FOR HIGH SUBSONIC FLOWMIYAZAKI T; HIRAYAMA N.1982; BULL. JSME; ISSN 0021-3764; JPN; DA. 1982; VOL. 25; NO 201; PP. 342-348; BIBL. 9 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

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

EINFACHES UMBEWERTUNGSVERFAHREN FUER DIE GESCHWINDIGKEITSVERTEILUNG AUF BELIEBIGEN GITTERPROFILEN KLEINEN TEILUNGSVERHAELTNISSES = METHODE SIMPLE D'EVALUATION POUR LA DISTRIBUTION DE VITESSE SUR DES CASCADES DE PROFILS QUELCONQUES AVEC FAIBLE ESPACEMENTHACKESCHMIDT M.1981; MASHINENBAUTECHNIK; ISSN 0025-4495; DDR; DA. 1981; VOL. 30; NO 6; PP. 279-281; ABS. ENG/RUS; BIBL. 5 REF.Article

SIMULATION MATHEMATIQUE SUR ORDINATEUR D'UN ECOULEMENT STATIONNAIRE ET NON STATIONNAIRE DE FLUIDE PARFAIT INCOMPRESSIBLE AUTOUR DES AILES ET CASCADESKOTOVSKIJ VN; NISHT MI; FEDOROV RM et al.1980; DOKL. AKAD. NAUK SSSR; ISSN 0002-3264; SUN; DA. 1980; VOL. 252; NO 6; PP. 1341-1345; BIBL. 9 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

UNIFIED UNSTEADY SUPERSONIC/HYPERSONIC THEORY OF FLOW PAST DOUBLE WEDGE AIRFOILSHUI WH.1983; ZEITSCHRIFT FUER ANGEWANDTE MATHEMATIK UND PHYSIK; ISSN 0044-2275; CHE; DA. 1983; VOL. 34; NO 4; PP. 458-486; ABS. FRE; BIBL. 14 REF.Article

TRANSONIC FLOW PAST OSCILLATING AIRFOILSTIJDEMAN H; SEEBASS R.1980; ANNU. REV. FLUID MECH.; USA; DA. 1980; VOL. 12; PP. 181-222; BIBL. 3 P.Article

TRANSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON AN OSCILLATING AIRFOILDAVIS SS; MALCOLM GN.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 11; PP. 1306-1312; BIBL. 27 REF.Article

SECOND ORDER ACCURATE CALCULATION OF TRANSONIC FLOW OVER TURBOMACHINERY CASCADESIVES DC; LIUTERMOZA JF.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1149; 9 P.; BIBL. 14 REF.Conference Paper

AERODYNAMIC FORCE AND MOMENT ON OSCILLATING AIRFOILS IN CASCADEATASSI H; AKAI TJ.1978; GAS TURBINE CONFERENCE/1978-04-09/LONDRES; USA; NEW YORK: ASME; DA. 1978; 12 P.; BIBL. 17 REF.Conference Paper

THE DEVELOPMENT OF THERMAL BOUNDARY LAYERS IN AIRFOIL-CASCADE FLOWS WITH OFF-DESIGN ANGLES OF ATTACKZYSINA MOLOZHEN LM; DERGACH AA.1981; HEAT TRANSFER. SOVIET RESEARCH; ISSN 0440-5749; USA; DA. 1981 PUBL. 1982; VOL. 13; NO 5; PP. 36-42; BIBL. 5 REF.Article

EXPERIMENTS IN UNSTEADY TRANSSONIC FLOWDAVIS SS; MALCOLM GN.1979; STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE. 20/1979/ST LOUIS MO; USA; DA. 1979; VOL. 2; PP. 192-208; BIBL. 26 REF.Conference Paper

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