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Premiers essais de profil d'aile en régime cryogénique à la soufflerie T2 de l'ONERA/CERT = First cryogenic tests of an airfoil in ONERA/CERT T2 wind tunnelMICHEL, R; MIGNOSI, A.La Recherche aérospatiale. 1984, Num 2, pp 149-151, issn 0034-1223Article

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

Strömungstechnische Untersuchungen an einem Düse-Heck-Modell = Wood-tunnel testing at a nozzle-tail modelDETSCH, F.Wissenschaftliche Zeitschrift der Technischen Universität Dresden. 1995, Vol 44, Num 3, pp 35-39, issn 0043-6925Article

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

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

A rational method to choose optimum design for two-dimensional contractionsRAMASESHAN, S; RAMASWAMY, M. A.Journal of fluids engineering. 2002, Vol 124, Num 2, pp 544-546, issn 0098-2202Article

Constructing an hydrodynamic/arodynamic research tunnelWILSON, P. A; SMITHWICK, E. T.Naval architect. 1995, Num JULAOU, pp E434-E436, issn 0306-0209, 2 p.Article

Effect of screen porosity and location on wind-tunnel turbulenceREFAI AHMED, G; BRUNDRETT, E.AIAA journal. 1995, Vol 33, Num 5, pp 958-960, issn 0001-1452Article

ETW aerodynamic design : A case studyBOUIS, X; PRIEUR, J; TIZARD, J. A et al.AGARD conference proceedings. 1997, pp 11.1-11.13, issn 0549-7191, isbn 92-836-0042-8Conference Paper

Neige et soleil à volonté = Snow and sun at willDEGREVE, I.Revue pratique du froid et du conditionnement d'air. 1995, Num 817, pp 24-25, issn 0370-6699Article

Aerodynamics life at Reynolds numbers below 7 × 104LAITONE, E. V.AIAA journal. 1996, Vol 34, Num 9, pp 1941-1942, issn 0001-1452Conference Paper

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

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

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

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

Aerodynamics of a triangular jib and boom combinationJAHKOLA, M.Journal of wind engineering and industrial aerodynamics. 1985, Vol 19, Num 1-3, pp 351-361, issn 0167-6105Article

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

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