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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

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

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

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

AN OPTO-ELECTRONIC METHOD FOR WIND TUNNEL MODEL ALIGNMENTJETT GB.1980; INSTRUMENTATION IN THE AEROSPACE INDUSTRY. ADVANCES IN TEST MEASUREMENT. INTERNATIONAL INSTRUMENTATION SYMPOSIUM. 26/1980/SEATTLE WA; USA; RESEARCH TRIANGLE PARK NC: INSTRUMENT SOCIETY OF AMERICA; DA. 1980; VOL. 1; PP. 379-392; BIBL. 2 REF.Conference Paper

ACOUSTICS LOADS ON UPPER-SURFACE-BLOWN POWERED-LIFT SYSTEMS.WILLIS CM; SCHOENSTER JA; MIXSON JS et al.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 10; PP. 670-675; BIBL. 13 REF.Article

A NEW ELECTRONIC SCANNER OF PRESSURE DESIGNED FOR INSTALLATION IN WIND-TUNNEL MODELSCOE CF; PARRA GT; KAUFFMAN RC et al.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. 17-24; BIBL. 7 REF.Conference Paper

REVIEW OF WIND-TUNNEL FREESTREAM PRESSURE FLUCTUATIONS.LADERMAN AJ.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 605-608; BIBL. 20 REF.Article

LASER MEASUREMENT OF ANGLE OF ATTACK ON WIND-TUNNEL MODELSPOND CR; HILL EG.1981; ASTRONAUT. AERONAUT.; ISSN 0004-6213; USA; DA. 1981; VOL. 19; NO 1; PP. 56-79; 3 P.; BIBL. 2 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

A SIMPLE OMNIDIRECTIONAL SENSOR FOR WIND-TUNNEL STUDIES OF PEDESTRIAN-LEVEL WINDSIRWIN HPAH.1981; J. WIND ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 7; NO 3; PP. 219-239; BIBL. 8 REF.Article

COMPARATIVE MEASUREMENTS IN FOUR EUROPEAN WIND TUNNELS OF THE UNSTEADY PRESSURES ON AN OSCILLATING MODELKIENAPPEL K; LAMBOURNE NC; DESTUYNDER R et al.1980; FORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT RAUMFAHRT; DEU; DA. 1980; NO 30; 128 P.; ABS. GER; BIBL. 7 REF.Serial Issue

A LASER-INTERFEROMETRIC TRAJECTORY-FOLLOWING SYSTEM FOR DETERMINING FORCES ON FREELY FLYING MODELS IN A SHOCK-TUNNELBERNSTEIN L; STOTT GT.1982; SHOCK TUBES AND WAVES. INTERNATIONAL SYMPOSIUM ON SHOCK TUBES AND WAVES. 13 /1981-07-06/NIAGARA FALLS NY; USA; ALBANY: STATE UNIVERSITY OF NEW YORK PRESS; DA. 1982; PP. 150-158; BIBL. 12 REF.Conference Paper

AN IMPROVED METHOD FOR CALCULATING ISENTROPIC TRANSONIC FLOWS IN TWO-DIMENSIONAL TURBINE CASCADES OF ARBITRARY SMOOTH PROFILESSTERN J.1982; ACTA TECH. CSAV; ISSN 0001-7043; CSK; DA. 1982; VOL. 27; NO 5; PP. 546-562; BIBL. 9 REF.Article

AERODYNAMIC CHARACTERISTICS OF A SLOTTED VS SMOOTH-SKIN SUPERCRITICAL WING MODELGROSSER WF.1983; JOURNAL OF AIRCRAFT; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 1; PP. 92-96; BIBL. 5 REF.Article

ESSAIS DE MOQUETTES DE TUYERES VENTILEES A FLUX PRIMAIRE SUPERSONIQUEPAULON J; PERUCCHINI J.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 3; PP. 217-221; BIBL. 6 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

DESIGN OF A PROTOTYPE SKIN-FRICTION TRANSDUCER AND WIND TUNNEL TEST RESULTSEAVES RH JR; LEDFORD RL.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 74-78; BIBL. 4 REF.Conference Paper

QUELQUES AMELIORATIONS DANS LA DETERMINATION DES TRANSFERTS CONVECTIFS A PARTIR DE LA THERMOGRAPHIE INFRAROUGEBALAGEAS DL; ORY D.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 3; PP. 213-219; ABS. ENG; BIBL. 3 REF.Article

UNTERSUCHUNG DER REIBUNGSBEHAFTETEN UMSTROEMUNG AN SCHIFFSDOPPELMODELLEN IM WINDKANAL = ETUDE DE L'ECOULEMENT AVEC FROTTEMENT AUTOUR DE MAQUETTES DOUBLES DE BATEAU EN SOUFFLERIEHAUKE W.1979; SCHR.-REIHE ZENTRALINST. MATH. MECH. AKAD. WISSENSCH. D.D.R.; DDR; DA. 1979; VOL. 28; PP. 83-122; BIBL. 27 REF.Article

EXPERIMENTAL STUDY OF THE INFLUENCE OF SUPPORTS ON THE AERODYNAMIC LOADS ON AN OGIVE CYLINDER AT HIGH ANGLES OF ATTACKCANNING TN; NIELSEN JN.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 7 P.; BIBL. 5 REF.Conference Paper

PROBLEMES DE CONSTRUCTION DE MAQUETTES POUR LES SOUFFLERIES A GRAND NOMBRE DE REYNOLDSBAZIN M.1978; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FRA; DA. 1978; NO 6; PP. 1-35; ABS. ENG; BIBL. 59 REF.Serial Issue

The use of aeroelastic wind tunnel models to prove structural designHOENLINGER, H; SCHWEIGER, J; SCHEWE, G et al.AGARD conference proceedings. 1987, Num 403, pp 9.1-9.15, issn 0549-7191Conference 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

Particularité de l'écoulement hypersonique autour de maquettes dans des souffleries de différentes classesALFEROV, V. I; LABAZKIN, A. P; RUDAKOVA, A. P et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1986, Num 2, pp 181-184, issn 0568-5281Article

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