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Results 1 to 25 of 1135

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EFFETTO DELLO SPESSORE NEL CALCOLO DI FORZE AERODINAMICHE GENERALIZZATE SU UN' ALA OSCILLANTE. = EFFET DE L'EPAISSEUR SUR LE CALCUL DES FORCES AERODYNAMIQUES GENERALISEES SUR UNE AILE OSCILLANTESANTINI P; CARLINI O; OGNIBENE L et al.sdIN: SATELL. METEOROL. RISORSE TERREST. TECNOL. SPEC. COLLAB. INT. ATTI XIV CONV. INT. SPAZIO; ROMA; 1974; ROMA; RASSEGNA INT. ELETTRON. NUCL. AEROSP.; DA. S.D.; PP. 153-159; ABS. ANGL.; BIBL. 3 REF.Conference Paper

DETERMINATION DES MOMENTS DES FORCES AERODYNAMIQUES S'EXERCANT SUR LES CORPS TRIDIMENSIONNELS SOUMIS A UN ECOULEMENT DANS LES CONDITIONS DE LA LOI DE LOCALISATIONVOROTYNTSEV MA; SAZONOVA NI.1976; VEST. MOSKOV. UNIV., 1; S.S.S.R.; DA. 1976; VOL. 31; NO 1; PP. 104-109; ABS. ANGL.; BIBL. 5 REF.Article

BERICHT UEBER DIE SITZUNG DES DGLR-FACHAUSSCHUSSES 3.4 VERSUCHSWESEN IN DER STROEMUNGSMECHANIK AM 5.6.1973 IN BREMEN. DIE MESSUNG VON TEILKRAEFTEN AN WINDKANALMODELLEN. = RAPPORT DU CONGRES DU COMITE SCIENTIFIQUE 3.4 DU DGLR SUR "LES TECHNIQUES EXPERIMENTALES DE LA MECANIQUE DES FLUIDES", DU 5 JUIN 1973 A BREME. MESURE DES FORCES SUR LES PARTIES DES MODELES MIS EN SOUFFLERIE AERODYNAMIQUE)EWALD B; KOPPENWALLNER G.1975; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1975; VOL. 75; NO 2; PP. 1-198; ABS. ANGLArticle

THE EFFECT OF TRAILING-EDGE STRIPS ON THE UNSTEADY AERODYNAMIC FORCES ON A CONTROL SURFACELONG G; FARRELL PA.1980; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1980; VOL. 84; NO 838; PP. 388-391; BIBL. 5 REF.Article

CALCUL ANALYTIQUE DES CARACTERISTIQUES AERODYNAMIQUES DE CORPS DE REVOLUTION DANS LES CONDITIONS DE LA LOI DE LOCALITEBUNIMOVICH AI; CHISTOLINOV VG.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 5; PP. 94-100; BIBL. 6 REF.Article

SCRUTON NUMBER: A PROPOSALZDRAVKOVICH MM.1982; J. WIND ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1982; VOL. 10; NO 3; PP. 263-265; BIBL. 19 REF.Article

COMPUTATION OF AERODYNAMIC LOADS ON HELICOPTER ROTORBLADES IN FOR WARD FLIGHT, USING THE METHOD OF THE ACCELERATION POTENTIAL.VAN HOLTEN T.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 323-334; BIBL. 2 REF.Book Chapter

EXPERIMENTAL INVESTIGATION OF WING-TIP VORTEX ABATEMENT.YUAN SW; BLOOM AM.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 303-311; BIBL. 8 REF.Conference Paper

GOLF BALL AERODYNAMICS.BEARMAN PW; HARVEY JK.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 2; PP. 112-122; BIBL. 6 REF.Article

AERODYNAMIC FORCE ACTING ON A CIRCULAR CYLINDER WITH TANGENTIAL INJECTION OF AIR.FURUYA Y; YOSHINO F.1975; BULL. J.S.M.E.; JAP.; DA. 1975; VOL. 18; NO 123; PP. 1002-1010; BIBL. 15 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

CATASTROPHIC LIFT FORCES ON RACING CARSHOWELL J.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 145-154; BIBL. 4 REF.Conference Paper

EMPIRICAL ESTIMATES OF GUST LOADS ON FINITE WINGSPATEL MH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 12; PP. 1602-1604; BIBL. 7 REF.Article

INSTATIONAERE LUFTKRAEFTE AN TRAGFLAECHEN MIT SCHWINGENDEM RUDER = FORCES AERODYNAMIQUES INSTATIONNAIRES SUR DES SURFACES PORTANTES AVEC VOLETS OSCILLANTSGEISLLER W.1980; JAHRB. DTSCH. GES. LUFT-RAUMFAHRT E.V. DGLR; ISSN 0070-4083; DEU; DA. 1980 PUBL. 1981; VOL. 1; PP. 031.1-031.28; BIBL. 15 REF.Article

A METHOD FOR CALCULATING THE AERODYNAMIC FORCES AND MOMENTS ON EXTERNAL STORES OF AIRCRAFTRONEN T; HANIN M.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 176-181; BIBL. 11 REF.Conference Paper

CARACTERISTIQUES DE TREMBLEMENT DE DEUX TYPES DE PROFILS SUBSONIQUES.TENSI J; LI FANG TSEN.1975; C.R. ACAD. SCI., B; FR.; DA. 1975; VOL. 281; NO 11; PP. 149-152; ABS. ANGL.; BIBL. 7 REF.Article

WHIRLING CABLE SUBJECTED TO VISCOUS DRAG. = CABLE EN ROTATION SOUMIS A UNE TRAINEE VISQUEUSERUSSELL JJ; ANDERSON WJ.1974; IN: FINITE ELEM. METHODS ENG. PROC. INT. CONF.; KENSINGTON, AUST.; 1974; KENSINGTON; UNISEARCH LTD.; DA. 1974; PP. 661-676; BIBL. 7 REF.Conference Paper

FORCE AND PRESSURE MEASUREMENTS ON AN AIRFOIL OSCILLATING THROUGH STALL.PARKER AG.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 10; PP. 823-827; BIBL. 13 REF.Article

A MODEL FOR THE EVALUATION OF INDUCED ROLLING MOMENTS AND SIDE FORCES IN SLENDER CRUCIFORM CANARD CONFIGURATIONS AT SMALL ANGLES OF INCIDENCE.GUR I; SHINAR J; ROM J et al.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 74-85; BIBL. 18 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper

METHODE DE CALCUL PRELIMINAIRE DE LA STABILITE DES CONSTRUCTIONS AERONAUTIQUESVASIL'EV YU V.1975; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1975; VOL. 20; NO 2; PP. 297-309; BIBL. 13 REF.Article

MOMENT DES FORCES DE RESISTANCE AERODYNAMIQUE PAR RAPPORT AUX AXES DE SUSPENSION DE GYROSCOPEPOTEMKIN A EH.1974; IZVEST. VYSSH. UCHEBN. ZAVED., PRIBOROSTR.; S.S.S.R.; DA. 1974; VOL. 17; NO 11; PP. 95-98; BIBL. 5 REF.Article

APPLICATION TO THE VIGGEN AIRCRAFT CONFIGURATION OF THE POLAR COARDINATE METHOD FOR UNSTEADY SUBSONIC FLOW.STARK VJE.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 312-322; BIBL. 10 REF.Book Chapter

WIE WIRKEN STROEMUNGSKRAEFTE VORBEIFAHRENDER FAHRZEUGE AUF MENSCHEN = INFLUENCE SUR L'HOMME DES FORCES AERODYNAMIQUES PRODUITES PAR LES VEHICULES A GRANDE VITESSEMULLER J.1973; EISENBAHNTECHNIK; DTSCH.; DA. 1973; VOL. 21; NO 5; PP. 218-219; ABS. RUSSE ANGL. FR.; BIBL. 1 REF.Serial Issue

REFINED PREDICTION METHOD FOR SUPERSONIC NONSTEADY AERODYNAMICS WITH AIC PARTITION SCHEMEII JM.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 8; PP. 609-617; BIBL. 13 REF.Article

REVIEW OF VORTEX-INDUCED ASYMMETRIC LOADS. IIERICSSON LE; REDING JP.1981; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1981; VOL. 5; NO 6; PP. 349-366; ABS. GER; BIBL. 94 REF.Article

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