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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

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

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

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

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

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

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

IMPACT DE L'INFORMATIQUE SUR LES ESSAIS EN SOUFFLERIECHEVALLIER JP.1982; MECANIQUE ET INFORMATIQUE. ASSOCIATION UNIVERSITAIRE DE MECANIQUE. JOURNEES/1982-09-16/CACHAN; FRA; CACHAN: ENSET; DA. 1982; PP. 1-14; BIBL. 4 REF.Conference Paper

MEASUREMENTS OF FLOW QUALITY IN THE AMES 2 X 2 FT TRANSONIC WIND TUNNELOWEN FK.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 6 P.; BIBL. 2 REF.Conference Paper

SIMULATION OF PLUME RISE USING SMALL WIND-TUNNEL MODELSPOREH M; KACHERGINSKY A.1981; J. WIND ENG. IND. AERODYN.; NLD; DA. 1981; VOL. 7; NO 1; PP. 1-14; BIBL. 19 REF.Article

THE DEVELOPMENT OF A SELF-STREAMLINING FLEXIBLE WALLED TRANSONIC TEST SECTIONGOODYER MJ; WOLF SWD.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 325-335; BIBL. 9 REF.Conference Paper

BOUNDARY LAYER CONTROLS ON THE SIDEWALLS OF WIND TUNNELS FOR TWO-DIMENSIONAL TESTSCHAN YY.1980; J. AVICR.; USA; DA. 1980; VOL. 17; NO 5; PP. 380-382; BIBL. 8 REF.Article

SIMPLIFIED SCULPTURED-SURFACE TECHNIQUE APPLIED TO WIND-TUNNEL MODELS.ROCHE M.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 735-736; BIBL. 1 REF.Article

TECHNIQUE FOR THE EVALUATION OF WALL INTERFERENCE AT TRANSONIC SPEEDSBAILEY AB; MILLER DG.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 2; PP. 245-246; BIBL. 5 REF.Article

THE EFFECT OF AN EMBANKMENT ON THE WIND STRUCTUREKILICKAYA MS.1980; D.I.S.A. INFORM.; DNK; DA. 1980; NO 25; PP. 10-14; ABS. GER/FRE; BIBL. 8 REF.Article

ANWENDUNG DER TIEFTEMPERATURTECHNIK IM STROEMUNGSTECHNISCHEN VERSUCHSWESEN. = APPLICATION DE LA CRYOGENIE DANS LES ESSAIS DE MECANIQUE DES FLUIDESHOTTNER T.1978; INGR-ARCH.; DEU; DA. 1978; VOL. 47; NO 4; PP. 241-256; ABS. ENG; BIBL. 13 REF.Article

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