The european transonic wind-tunnel ETW: A cryogenic solutionHARTZUIKER, J. P.Aeronautical Journal. 1984, Vol 88, Num 879, pp 379-394, issn 0001-9240Article

Développement des travaux suscités par les réalisations et les projets de souffleries cryogéniques = Developments in research stimulated by cryogenic wind tunnel construction planning and projectsCHRISTOPHE, J; BAZIN, M; BROUSSAUD, P et al.La Recherche aérospatiale. 1984, Num 2, pp 105-124, issn 0034-1223Article

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

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

A flying superconducting magnet and cryostat for magnetic suspension of wind-tunnel modelsBRITCHER, C; GOODYER, M. J; SCURLOCK, R. G et al.Cryogenics (Guildford). 1984, Vol 24, Num 4, pp 185-189, issn 0011-2275Article

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

Surface roughness studies for wind tunnel models used in high Reynolds number testingVORBURGER, T. V; MCLAY, M. J; SCIRE, F. E et al.Journal of aircraft. 1986, Vol 23, Num 1, pp 56-61, issn 0021-8669Article

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

Caractérisation des capteurs de pression destinés aux futures souffleries cryogéniques = Caracterization of pressure transducers for future cryogenic vind tunnelsPORTAT, M; HELIAS, F.La Recherche aérospatiale. 1983, Num 6, pp 413-418, issn 0034-1223Article

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

Cryogenic wind tunnel research: a global perspectiveDRESS, D. A; KILGORE, R. A.Cryogenics (Guildford). 1988, Vol 28, Num 1, pp 10-21, issn 0011-2275Article

Refinement of an alternate method for measuring heating rates in hypersonic wind tunnelsMILLER, C. G.AIAA journal. 1985, Vol 23, Num 5, pp 810-812, issn 0001-1452Article

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

Wind tunnels and testing techniques:/papers and discussions AGARD Fluid Dynamics Panel symposium, Çesme, Turkey, 26-29 september 1983AGARD conference proceedings. 1984, Num 348, issn 0549-7191, pag. multConference Proceedings

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

Rapid valve opening technique for supersonic blowdown tunnelLU, F. K; WILSON, D. R; MATSUMOTO, J et al.Experimental thermal and fluid science. 2009, Vol 33, Num 3, pp 551-554, issn 0894-1777, 4 p.Article

Investigations of transonic Ludwieg tubes. III: Effects of plenum exhaust system on starting process of tunnel test sectionKAGE, K; MATSUO, K; KAWAGOE, S et al.Bulletin of the JSME. 1985, Vol 28, Num 243, pp 1868-1873, issn 0021-3764Article

AERODYNAMIC BEHAVIOUR OF A SLENDER SLOT IN A WIND TUNNEL WALLBLISS DB.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 9; PP. 1244-1252; BIBL. 8 REF.Article

PROBLEMS OF TEMPERATURE COMPENSATION DURING DIRECT MEASUREMENT OF AERODYNAMIC PRESSURESGATZEK W.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. 6-16; BIBL. 5 REF.Conference Paper

VIBRATIONS DE MAQUETTES AU-DELA DU DECROCHAGE A BASSE VITESSEVAUCHERET X.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 6; PP. 387-397; 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