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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

COMPARISON OF NASA HELIUM TUNNEL TRANSITION DATA WITH NOISE-TRANSITION CORRELATION.PATE SR.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1615; BIBL. 4 REF.Article

PROGRES RECENTS DANS LES ETUDES EXPERIMENTALES D'ARRIERE-CORPS.MECHIN B.1975; AERONAUT. ET ASTRONAUT.; FR.; DA. 1975; NO 50; PP. 27-33; ABS. ANGL. ALLEM.; BIBL. 7 REF.Article

THREE-DIMENSIONAL AIRFLOW VISUALIZATION BY SMOKE TUNNELODA N; HOSHINO T.1974; S.A.E. TRANS.; U.S.A.; DA. 1974; VOL. 83; NO PART. 4; PP. 3187-3201; BIBL. 7REF.Article

GALLERIA DEL VENTO PININFARINA. I: STUDIO E PROGETTO. II: STRUMENTI DI MISURA = LA SOUFFLERIE PININFARINA. I: ETUDE ET PROJET. II: INSTRUMENTS DE MESUREMORELLI A; CERUTI G; PFISTER F et al.1974; A.T.A.; ITAL.; DA. 1974; VOL. 27; NO 3; PP. 113-136; ABS. ANGL.; BIBL. 25 REF.Article

ESSAI DE FILTRAGE NUMERIQUE EN TEMPS REEL A LA SOUFFLERIE CONTINUE S1 DE MODANEAPPEL J.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 5; PP. 347-351; ABS. ENG; BIBL. 1 REF.Article

MESURES EN VOL ET EN SOUFFLERIE SUR LE BORD D'ATTAQUE D'UNE AILE DE NORD 2501.COULOMB J; LEDOUX M; LERAT J et al.1978; AERONAUT. ET ASTRONAUT.; FR.; DA. 1978; NO 69; PP. 19-28; ABS. ANGL. ALLEM.; BIBL. 4 REF.Article

VEHICLE DYNAMICS AND HANDLING QUALITIES1975; IN: AM. INST. AERONAUT & ASTRON. SYMP. AERODYN. SPORTS & COMPETITION AUTOMOB. 2. PROC.; LOS ANGELES, CALIF.; 1974; LOS ANGELES, CALIF.; AM. INST. AERONAUT. ASTRON.; DA. 1975; PP. 148-164; BIBL. DISSEM.Conference Paper

INFLUENCE DE LA CHARGE DUE AU VENT SUR LA FORME D'UNE ANTENNE BALLISTIQUEKURKIN VI; MIROSHNIK RA.1974; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; S.S.S.R.; DA. 1974; NO 5; PP. 18-21; BIBL. 5 REF.Article

TRAILING VORTEX WIND-TUNNEL DIAGNOSTICS WITH A LASER VELOCIMETER.ORLOFF KL.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 477-482; BIBL. 22 REF.Article

UN VENT NOUVEAU A SOUFFLE SUR LE PROTOTYPE "CR 25" PININFARINA1974; BELG. AUTOM.; BELG.; DA. 1974; NO 12; PP. 9-11 (2 P.)Article

FLOW FIELD ANALYSIS1975; IN: AM. INST. AERONAUT. & ASTRON. SYMP. AERODYN. SPORTS & COMPETITION AUTOMOB. 2. PROC.; LOS ANGELES, CALIF.; 1974; LOS ANGELES, CALIF.; AM. INST. AERONAUT. ASTRON.; DA. 1975; PP. 99-147; BIBL. DISSEM.Conference Proceedings

DRAG REDUCTION OF TRAILER-TRACTOR CONFIGURATION BY AERODYNAMIC MEANSWONG HY; COX RN; RAJAN A et al.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 101-111; BIBL. 6 REF.Conference Paper

AN ANALYTICAL AND EXPERIMENTAL STUDY OF THE STEADY AND UNSTEADY AIRLOADS ON A WING OSCILLATING CONTROL INCLUDING A STREAMLINED GAPGEISSLER W.1981; GORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT-RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1981; VOL. 18; PP. 1-51; ABS. GER; BIBL. 6 REF.Serial Issue

EFFECTS OF CROSSWINDS ON VEHICLE RESPONSE. FULL-SCALE TESTS AND ANALYTICAL PREDICTIONSKLEIN RH; HOGUE JR.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; VOL. 89; NO 3; PP. 2578-2590; BIBL. 12 REF.Article

EMPIRICAL METHOD FOR PREDICTING THE MAGNUS CHARACTERISTICS OF SPINNING SHELLS.GRAFF GY; MOORE FG.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 10; PP. 1379-1380; BIBL. 5 REF.Article

HIGH ANGLE-OF-ATTACK AERODYNAMICS ON A SLENDER BODY WITH A JET PLUME.NELSON RC; FLEEMAN EL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 12-16; BIBL. 8 REF.Article

NATURE DE L'INFLUENCE DU NOMBRE DE REYNOLDS UNITAIRE SUR LA TRANSITION DANS UNE COUCHE LIMITE HYPERSONIQUEKHARITONOV AM; CHERNYKH VV.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 150-153; BIBL. 11 REF.Article

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

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

BOEENBEEINFLUSSUNG SCHNELLFAHRENDER ZUEGE = INFLUENCE DES RAFALES SUR LES TRAINS A GRANDE VITESSENEPPERT H; SANDERSON R.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 3; PP. 151-161; ABS. ANGL. FR.; BIBL. 12 REF.Article

AERODYNAMISCHE FORMOPTIMIERUNG VON VW GOLF UND VW SCIROCCO = OPTIMISATION DES FORMES AERODYNAMIQUES DES VOLKSWAGEN GOLF ET SCIROCCOJANSSEN LJ; HOCHO WH.1975; AUTOM.-TECH. Z.; DTSCH.; DA. 1975; VOL. 77; NO 11; PP. 309-313; ABS. ANGL.; BIBL. 5REF.Article

SOME AERODYNAMIC ASPECTS OF SAFETY IN ROAD VEHICLESCARR GW; ROSE MJ; SMITH NP et al.1973; INST. MECH. ENGRS, PROC.; G.B.; DA. 1973; VOL. 187; NO 30; PP. 333-360; BIBL. 29 REF.Serial Issue

COLLISION LESS PLASMA FLOW OVER A CONDUCTING SPHERESTONE NH; ORAN WA; URI SAMIR et al.1972; PLANET. SPACE SCI.; G.B.; DA. 1972; VOL. 20; NO 10; PP. 1787-1790; BIBL. 8 REF.Serial Issue

ZUR KINEMATIK EINER NACHLAUFSTROEMUNG = CINEMATIQUE D'UN SILLAGEWIEGHARDT K.1983; ZEITSCHRIFT FUER FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG; ISSN 0342-068X; DEU; DA. 1983; VOL. 7; NO 3; PP. 149-159; ABS. ENG; BIBL. 5 REF.Article

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