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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

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

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

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

Closed-loop Mach number control in a transonic wind-tunnelPELS, A. F.Journal A. 1989, Vol 30, Num 4, pp 25-32, issn 0771-1107, 8 p.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

Transonic wind tunnel wall interference minimizationGRUNNET, J. L.Journal of aircraft. 1984, Vol 21, Num 9, pp 694-699, issn 0021-8669Article

Condensation spontanée de l'azote dans une tuyère plane d'une soufflerie cryogéniqueSALTANOV, G. A; SIMANOVSKIJ, G. P; CHIRIKHIN, A. V et al.Prikladnaâ mehanika i tehničeskaâ fizika. 1984, Num 6, pp 97-101, issn 0869-5032Article

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

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

On the design of three-dimensional wind tunnel contractionsDOWNIE, J. H; JORDINSON, R; BARNES, F. H et al.Aeronautical Journal. 1984, Vol 88, Num 877, pp 287-295, issn 0001-9240Article

Code des singularités surfaciques pour calcul d'effets de parois et de supports de formes quelconques sur des maquettes en soufflerie = Vortex lattice code for computation of any wird tunnel and support effects on modelsVAUCHERET, X.La Recherche aérospatiale. 1991, Num 2, pp 39-51, issn 0034-1223, 13 p.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

The impulse transonic wind tunnel U-11. New effective technology for generation of sub-, trans- and supersonic gas flowKISLYKH, V. V; KOUDRIAVTSEV, V. V; PETROVA, O. V et al.AGARD conference proceedings. 1997, pp 14.1-14.13, issn 0549-7191, isbn 92-836-0042-8Conference Paper

Détermination des pertubations des champs d'écoulements des souffleries supersoniques d'après les valeurs mesurées des coefficients aérodynamiquesEREMIN, V. V; LIPNITSKIJ, YU. M; FILIPPOV, S. E et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1988, Num 5, pp 183-185, issn 0568-5281Article

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

Experiments and analysis for a gust generator in a wind tunnelTANG, D. M; CIZMAS, P. G. A; DOWELL, E. H et al.Journal of aircraft. 1996, Vol 33, Num 1, pp 139-148, issn 0021-8669Article

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

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

Applications of adaptive-wall wind tunnelsDAVIS, S. S.Journal of aircraft. 1986, Vol 23, Num 2, pp 158-160, issn 0021-8669Article

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

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