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Results 1 to 25 of 540

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CARACTERISTIQUES AERODYNAMIQUES D'UN ECOULEMENT PROVENANT D'UNE FENTEVISHNEVSKIJ EP.1975; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1975; VOL. 28; NO 5; PP. 915-916; RESUME DE L'ART. NO 3256-74 DEPOSE AU VINITIArticle

DIE AUSWERTUNG VON KRAFTMESSUNGEN AN FREIFLIEGENDEN MODELLEN IM GUN TUNNEL. = L'EXPLOITATION DE MESURES DE FORCES SUR DES MODELES EN VOL LIBRE EN SOUFFLERIEWYBORNY W.1976; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1976; VOL. 76; NO 10; PP. 1-44; ABS. ANGL.; BIBL. 9 REF.Serial Issue

PERFORMANCE OF A CASCADE THRUST REVERSER FOR SHORT-HAUL APPLICATIONS.DIETRICH DA; GUTIERREZ OA.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 3; PP. 185-191; BIBL. 9 REF.Article

REVIEW OF NASA SUPERCRITICAL AIRFOILS.WHITCOMB RT.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 8-18; BIBL. 21 REF.Conference Paper

MINIMISATION DE LA RESISTANCE DE CORPS EN ETOILE DANS UN ECOULEMENT HYPERSONIQUE DE GAZKRAVETS VV; NYIKOLAJEV SV.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 1; PP. 40-43; ABS. ANGL. RUSSE; BIBL. 2 REF.Article

AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING WITH A TIP CLEARANCE IN A CHANNEL.SUGIYAMA Y.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 4; PP. 541-547; BIBL. 8 REF.Article

AERODYNAMIC DESIGN OF HIGH-PERFORMANCE BIPLANE WINGS.ADDOMS RB; SPAID FW.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 8; PP. 629-630; BIBL. 2 REF.Article

APPLICATION DES LOIS DE SIMILITUDE GENERALISEES AU CALCUL DES CARACTERISTIQUES AERODYNAMIQUES DES CORPS TRIDIMENSIONNELSBUNIMOVICH AI; DUBINSKIJ AV.1976; VEST. MOSKOV. UNIV., 1; S.S.S.R.; DA. 1976; VOL. 31; NO 2; PP. 89-95; ABS. ANGL.; BIBL. 7 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES NON STATIONNAIRES DE GRILLES D'AUBES DE FORME ARBITRAIRERYABCHENKO VP.1976; PROBL. PROCHN., U.S.S.R.; S.S.S.R.; DA. 1976; NO 3; PP. 29-32; BIBL. 5 REF.Article

PROBLEME DE LA PENTE DES CARACTERISTIQUES DE PERFORMANCE D'UN COMPRESSEUR AXIALVORACEK V.1975; STROJN. CAS.; CESKOSL.; DA. 1975; VOL. 26; NO 2; PP. 142-155; ABS. RUSSE; BIBL. 4 REF.Article

A STATE-OF-THE ART SURVEY OF TWO-DIMENSIONAL AIRFOIL DATA.PROUTY RW.1975; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1975; VOL. 20; NO 4; PP. 14-25; BIBL. 32 REF.Article

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

SUBSONIC LOADS ON WINGS HAVING SHARP LEADING EDGES AND TIPS.KANDIL OA; MOOK DT; NAYFEH AH et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 62-63; BIBL. 10 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES NON STATIONNAIRES DE SYSTEMES PORTEURS TRIDIMENSIONNELSPOPYTALOV SA.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 173-176; BIBL. 8 REF.Article

DETERMINATION DES CARACTERISTIQUES AERODYNAMIQUES DES CORPS SOUMIS A UN ECOULEMENT DE TRANSLATION DANS LES CONDITIONS DE LA LOI DE LOCALISATIONBUNIMOVICH AI; VOROTYNTSEV MA; SAZONOVA NI et al.1975; VEST. MOSKOV. UNIV., 1; S.S.S.R.; DA. 1975; VOL. 13; NO 6; PP. 111-116; ABS. ANGL.; BIBL. 3 REF.Article

AUGMENTATION OF VORTEX LIFT BY SPANWISE BLOWING.CAMPBELL JF.1975; IN: AM. INST. AERONAUT. ASTRONAUT AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 993; PP. 1-6; H.T. 3; BIBL. 19 REF.Conference Paper

ON THE CALCULATION OF NON-LINEAR AERODYNAMIC CHARACTERISTICS AND THE NEAR VORTEX WAKE.ROM J; ZOREA C; GORDON R et al.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 214-228; BIBL. 1 P. 1/2Conference Paper

WING-ALONE AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACKSTALLINGS RL JR; LAMB M.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 7 P.; BIBL. 6 REF.Conference Paper

A WIND TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF FORWARD SWEPT WINGSWEEKS TM; UHUAD GC; LARGE R et al.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 15 P.Conference Paper

LA SIMULATION ELECTRIQUE DES CARACTERISTIQUES AERODYNAMIQUES DES VENTILATEURSVODYANIK GM; FEDICHKINA OI.1976; IZVEST. VYSSH. UCHEBN. ZAVED., ELEKTROMEKH.; S.S.S.R.; DA. 1976; NO 5; PP. 547-552; BIBL. 5 REF.Article

THE DEVELOPMENT OF THEORETICAL MODELS FOR JET-INDUCED EFFECTS ON V/STOL AIRCRAFT.SICLARI MJ; MIGDAL D; PALCZA JL et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1216; PP. 1-10; BIBL. 12 REF.Conference Paper

UNSTEADY TRANSONIC FLOWS OVER AN AIRFOIL.MAGNUS R; YOSHIHARA H.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1624-1628; BIBL. 8 REF.Article

AERODYNAMIC CHALLENGES FOR THE FASTER INTERFACE VEHICLES = FACTEURS AERODYNAMIQUES QUI INFLUENCENT LES VEHICULES AVANCES FONCTIONNANT DANS L'INTERFACE SOL-AIR ET MER-AIRSHIPPS PR.1973; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1973; VOL. 19; NO 2; PP. 53-59; BIBL. 10 REF.Serial Issue

SOME AERODYNAMIC DESIGN CONSIDERATIONS FOR HIGH BYPASS RATIO FANSSMITH LH JR.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (14 P.); BIBL. 5 REF.Conference Paper

SUBSONIC/TRANSONIC CONFIGURATION AERODYNAMICSKORNER HORST.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD-AR/146; 14 P.; 30 CM; BIBL. 29 REF.; ISBN 92-835-1380-0Report

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