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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

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

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

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

SEMISPAN MODEL TESTING IN A VARIABLE POROSITY TRANSONIC WIND TUNNELPOUNDS GA; WALKER J.1980; AERODYNAMICS TESTING CONFERENCE 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 336-343; BIBL. 11 REF.Conference Paper

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

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

SUPPORT INTERFERENCE IN STATIC AND DYNAMIC TESTSERICSSON LE; REDING JP.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. 213-223; BIBL. 18 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

LASER VELOCIMETER FOR LARGE WIND TUNNELSREINATH MS.1982; J. AICR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 12; PP. 1100-1102; BIBL. 4 REF.Article

DISPOSITIF A 6 DEGRES DE LIBERTE POUR L'ETUDE DES SEPARATIONS DE CHARGES DANS LES SOUFFLERIES DE L'ONERA.COSTE J.1978; AERONAUT. ET ASTRONAUT.; FR.; DA. 1978; NO 68; PP. 4-10; ABS. ANGL. ALLEM.Article

ANALYSIS OF BOUNDARY LAYERS ON PERFORATED WALLS OF TRANSONIC WIND TUNNELSCHAN YY.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 6; PP. 469-473; BIBL. 17 REF.Article

CRYOGENIC WIND TUNNELS1980; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1980; AGARD-LS/111; 280 P.; 30 CM; BIBL. DISSEM.; 92-835-1360-6Report

THE NATIONAL TRANSONIC FACILITY: STATUS AND OPERATIONAL PLANNINGHOWELL RR.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 1-9; BIBL. 4 REF.Conference Paper

EICHUNG DES HOCHGESCHWINDIGKEITSKANALS TVM 150 IM UEBERSCHALLBEREICH = ETALONNAGE DE LA SOUFFLERIE A GRANDE VITESSE TVM150 DANS LE DOMAINE SUPERSONIQUEWEINERT W.1980; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1980; VOL. 4; NO 5; PP. 280-289; ABS. ENG; BIBL. 20 REF.Article

A SURFACE FLOW VISUALISATION TECHNIQUE FOR USE IN CRYOGENIC WIND TUNNELSKELL DM.1978; AERONAUT. J.; GBR; DA. 1978; VOL. 82; NO 815; PP. 485-487; BIBL. 4 REF.Article

DYNAMIC STABILITY MEASUREMENTS FROM TUNNEL UNSTEADINESS EXCITED RANDOM RESPONSEMURTHY HS; JATEGAONKAR RV; BALAKRISHNA S et al.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 1; PP. 7-12; BIBL. 23 REF.Article

VERMESSUNG DES BOEENFELDES HINTER HARMONISCH SCHWINGENDEN BOEENERZEUGERN IM MODELL-UNTERSCHALL-KANAL (MUK) = MESURE DU CHAMP DE RAFALE DERRIERE DES GENERATEURS DE RAFALE A OSCILLATIONS HARMONIQUES DANS LA SOUFFLERIE SUBSONIQUE MODELEKRAG B.1982; FORSCHUNGSBERICHT- DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1982; NO 26; 145 P.; ABS. ENG; BIBL. 16 REF.Serial Issue

ADDITIONAL FLOW QUALITY MEASUREMENTS IN THE LANGLEY RESEARCH CENTER 8-FOOT TRANSONIC PRESSURE TUNNELBROOKS JD; STAINBACK PC; BROOKS CW JR et al.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 138-145; BIBL. 6 REF.Conference Paper

AN OSCILLATING RIG FOR THE GENERATION OF SINUSOIDAL FLOWSSTAPOUNTZIS H.1982; JOURNAL OF PHYSICS E: SCIENTIFIC INSTRUMENTS; ISSN 0022-3735; GBR; DA. 1982; VOL. 15; NO 11; PP. 1173-1176; BIBL. 19 REF.Article

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

DIE ZULAESSIGE MODELLGROESSE BEI MESSUNGEN IN FREISTRAHL-UEBERSCHALWINDKANAELEN = DIMENSION DE MODELE ADMISSIBLE DANS LES MESURES EN SOUFFLERIE SUPERSONIQUE A JET LIBREJUNGCLAUS G; KROHN EO.1982; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1982; VOL. 6; NO 5; PP. 348-350; ABS. ENG; BIBL. 5 REF.Article

METHODE DE MESURE DES FORCES LORS D'UN ESSAI EN SOUFFLERIE A IMPULSIONSVEDERNIKOV GA; ZVEGINTSEV VI.1981; IZV. SIB. OTD. AKAD. NAUK SSSR, SER. TEH. NAUK; ISSN 0002-3434; SUN; DA. 1981; NO 3; PP. 58-64; BIBL. 8 REF.Article

INVESTIGATION OF THE STARTING PROCESS OF A SUPERSONIC WIND TUNNELMATSUO K; SASAGUCHI K; MOCHIZUKI H et al.1980; BULL JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 186; PP. 1975-1981; BIBL. 11 REF.Article

SUPERSONIC FLOW DEVELOPMENT IN SLOTTED WIND TUNNELSRAMASWAMY MA; CORNETTE ES.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 165-171; BIBL. 2 REF.Conference Paper

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