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ADAPTATION ET PREMIER FONCTIONNEMENT CRYOGENIQUE DE LA SOUFFLERIE T2 DE L'ONERA/CERTMICHEL R; MIGNOSI A.1982; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1982; NO 2; PP. 131-141; ABS. ENG; BIBL. 5 REF.Article

RECENT ADVANCES IN THE PERFORMANCE AND TESTING CAPABILITIES OF THE AEDC-VKF TUNNEL F (HOTSHOT) HYPERSONIC FACILITY.PATE SR; EAVES RH JR.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 84; PP. 1-23; BIBL. 2 P.Conference Paper

LA SOUFFLERIE TRANSSONIQUE A INDUCTION T2: FONCTIONNEMENT A TEMPERATURE AMBIANTE ET ADAPTATION CRYOGENIQUEMIGNOSI A; FAULMANN D; SERAUDIE A et al.1981; RECT. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 3; PP. 203-215; ABS. ENG; BIBL. 9 REF.Article

LARGE WINDTUNNELS: REQUIRED CHARACTERISTICS AND THE PERFORMANCE OF VARIOUS TYPES OF TRANSONIC FACILITY.PANKHURST RC.1974; AGARD-R-615; FR.; DA. 1974; PP. (155P.); ABS. ANGL.; BIBL. DISSEM.Report

RECHERCHES SUR UNE SOUFFLERIE CRYOGENIQUE FONCTIONNANT PAR INDUCTIONBLANCHARD A; DOR JB; MIGNOSI A et al.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 2; PP. 127-141; ABS. ENG; BIBL. 6 REF.Article

SOME TUNNEL-WALL EFFECTS ON TRANSONIC FLUTTER.RUHLIN CL; DESTUYNDER RM; GREGORY RA et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 162-167; BIBL. 10 REF.Article

THREE YEARS OF OPERATION OF THE ONERA PRESSURIZED SUBSONIC WIND TUNNELCARRARA JM; MASSON A.sdICAS 1980. INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES. CONGRESS. 12/1980/MUNICH; USA; DA. S.D.; PP. 778-792; BIBL. 5 REF.Conference Paper

EXPERIMENTAL DETERMINATION OF ASYMMETRY-INDUCED TRIM ANGLES OF ATTACK = DETERMINATION EXPERIMENTALE DES ANGLES D'ATTAQUE DE TRIM INDUITS PAR DES ASYMETRIESCLARK EL JR; HODAPP AE JR.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-8; BIBL. 10 REF.Conference Paper

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

UEBERSCHALL-WINDKANAL M4 DES INSTITUTO FUER LUFT- UND RAUMFAHRT DER TECHNISCHEN HOCHSCHULE AACHEN. = SOUFFLERIE SUPERSONIQUE M4 DE L'INSTITUT POUR L'AERONAUTIQUE ET L'ASTRONAUTIQUE DE L'ECOLE TECHNIQUE SUPERIEURE D'AIX-LA-CHAPELLELANGEFELD W; HAAKE M.1974; DTSCHE LUFT- U. RAUMFAHRT, MITT.; DTSCH.; DA. 1974; NO 14; PP. 1-59; ABS. ANGL.; BIBL. 1 P.Article

WINDKANAELE IN DRESDEN LOESEN AUFGABEN FUER INDUSTRIE UND FORSCHUNG. = LES SOUFFLERIES DE DRESDE SERVENT A RESOUDRE DES PROBLEMES POUR L'INDUSTRIE ET LA RECHERCHEEIGEL J; BENNDORF D.1974; MASCHINENBAUTECHNIK; DTSCH.; DA. 1974; VOL. 23; NO 9; PP. 395-404 (7P.); ABS. RUSSE ANGL.; BIBL. 6 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

SIX-COMPONENT STRAIN-GAGE BALANCES FOR LARGE WIND TUNNELSDUBOIS M.1981; EXP. MECH.; ISSN 0014-4851; USA; DA. 1981; VOL. 21; NO 11; PP. 401-407; BIBL. 25 REF.Article

DEVELOPMENT OF A SELF-STREAMLINING FLEXIBLE WALLED TRANSONIC TEST SECTIONGOODYER MJ; WOLF SWD.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 2; PP. 227-234; BIBL. 21 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

SOME NOTES ON THE DESIGN, CONSTRUCTION AND PERFORMANCE OF THE LOW-SPEED WIND-TUNNEL AT ITB.HARIJONO DJOJODIHARDJO.1973; INST. TEKNOL. BANDUNG, PROC.; INDONES.; DA. 1973; VOL. 7; NO 3; PP. 103-118; ABS. INDONES.; BIBL. 3 REF.Article

VELOCIMETRIE LASER A S3 MODANEBOUTIER A.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 6; PP. 411-415; BIBL. 2 REF.Article

REMARQUES SUR L'ETUDE DES SOUFFLERIES SUPERSONIQUESZBIGNIEW D; KACZMARCZYK J; TARNOGRODZKI A et al.1978; ARCH. BUDOWY MASZ.; POLSKA; DA. 1978; VOL. 25; NO 1; PP. 285-294; ABS. RUSSE ANGL.; BIBL. 9 REF.Article

COMMANDE EN TEMPS REEL DU NOMBRE DE MACH DANS UNE SOUFFLERIE TRANSSONIQUE A RAFALES.GOBERT JL.1975; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1975; PP. 1-66; ABS. ANGL.; BIBL. 20 REF.; (THESE DOCT. 3E CYCLE; PARIS VI; 1975)Thesis

UEBERLEGUNGEN ZUM PROJEKT EINES AEROAKUSTIK-WINDKANALS. = CONSIDERATIONS SUR LE PROJET DE SOUFFLERIE AEROACOUSTIQUESCHULZ G.1974; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1974; NO 74-27; PP. 1-18; ABS. ANGL.; BIBL. 4 REF.Article

ARBEITEN DER DFVLR AUF DEM GEBIET DER KRYO-WINDKANAL-TECHNIK = TRAVAUX DE L'INSTITUT ALLEMAND DE RECHERCHE AEROSPATIALE DANS LE DOMAINE DE LA TECHNIQUE DE LA SOUFFLERIE CRYOGENIQUEVIEHWEGER G; LORENZ MEYER W.1980; DFVLR-NACHR.; ISSN 0011-4901; DEU; DA. 1980; NO 31; PP. 8-12Article

FLOW QUALITY IMPROVEMENTS IN A BLOWDOWN WIND TUNNEL USING A MULTIPLE SHOCK ENTRANCE DIFFUSERARNOLD JW; COOKSEY JM.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-11; BIBL. 8 REF.Conference Paper

WINDTUNNEL MEASUREMENTS WITH AN ELECTRONICALLY SCANNED MULTIPORT PRESSURE SENSOR SYSTEMMEYER C.1981; ICIASF'81. INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES/1981/DAYTON OH; USA; NEW YORK: THE INSTITUTE OF ELECTRICAL AND ELECTRONICS ENGINEERS; DA. 1981; PP. 1-5; BIBL. 7 REF.Conference Paper

EFFECTS OF SIDEWALL BOUNDARY LAYERS IN TWO-DIMENSIONAL SUBSONIC AND TRANSONIC WIND TUNNELSSEWALL WG.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 9; PP. 1253-1256; BIBL. 10 REF.Article

TOWARDS NEW TRANSONIC WINDTUNNELSHARTZUIKER JP ED.1979; ; FRA; DA. 1979; AGARD-AG 240; PAG. MULT.: ILL.; 30 CM; BIBL. DISSEM.; ISBN 92-835-1343-6Report

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