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Results 1 to 25 of 110

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AUTOMATISIERTE MESSWERTERFASSUNG BEI STROEMUNGSMESSUNGEN IM WINDKANAL. = ENREGISTREMENT AUTOMATIQUE DES RESULTATS DE MESURES EN SOUFFLERIEBEGER G; GERLACH K; HAUKE W et al.1974; MASCHINENBAUTECHNIK; DTSCH.; DA. 1974; VOL. 23; NO 9; PP. 410-413; ABS. RUSSE ANGL.Article

DYNAMIC STABILITY MEASUREMENTS FROM TUNNEL UNSTEADINESS EXCITED RANDOM RESPONSEMURTHY HS; JATEGAONKAR RV; BALAKRISHNA S et al.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 1; PP. 7-12; BIBL. 23 REF.Article

MISE EN OEUVRE DE TECHNOLOGIES NOUVELLES DANS LA FABRICATION D'ELEMENTS STRUCTURAUX DE MAQUETTESDUPRIEZ F; DESCHAMPS M; DRUEL J et al.1980; ; FRA; DA. 1980; DGRST/78 7 3064; 122 P.; 30 CM; ACTIONS URGENTESReport

DESIGN STUDY OF BASIC MODEL FOR USE IN THE PROPOSED 8 BY 10 FT. HIGH-REYNOLDS-NUMBER TRANSONIC WIND TUNNEL (HIRT) AT ARNOLD ENGINEERING DEVELOPMENT CENTER.ALEXANDER WK; GRIFFIN SA.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 82; PP. 1-10; BIBL. 6 REF.Conference Paper

ANALYSIS OF VALIDATION TEST OF THE LANGLEY PILOT TRANSONIC CRYOGENIC TUNNEL.RAY EJ; KILGORE RA; ADCOCK JB et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 6; PP. 539-544; BIBL. 4 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

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

THE MEASUREMENT OF IMPULSIVE FORCES ON A WIND TUNNEL MODEL WITH A CONVENTIONAL STRAIN GAGE BALANCECOOKSEY JM; ZIEGLER CE.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. 179-187; BIBL. 7 REF.Conference Paper

A SYSTEM FOR THE MEASUREMENT OF THE ATTITUDE OF WIND TUNNEL MODELSJEFFERY RW; TUCK AN; LAW RD et al.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 306-315; BIBL. 6 REF.Conference 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

WAERMEUEBERGANGSMESSUNGEN MIT FLUESSIYKRISTALLEN IM ROHRWINDKANAL IN GOETTINGEN = MESURES DE TRANSFERT DE CHALEUR A L'AIDE DE CRISTAUX LIQUIDES DANS LA SOUFFLERIE TUBULAIRE DE GOETTINGENSCHOELER H.1980; DFVLR-NACH.; ISSN 0011-4901; DEU; DA. 1980; NO 31; PP. 1-3Article

AERODYNAMIC OPTIMIZATION OF A GROUP-5 RACING CARGERHARDT HJ; KRAMER C.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 155-165; BIBL. 4 REF.Conference Paper

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

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

AERODYNAMIC DRAG AND PRESSURE MEASUREMENTS ON A SIMPLIFIED TRACTOR-TRAILER MODELALLAN JW.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 125-136; BIBL. 10 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

AN OPTO-ELECTRONIC METHOD FOR WIND TUNNEL MODEL ALIGNMENTJETT CB.1981; ISA TRANS.; ISSN 0019-0578; USA; DA. 1981; VOL. 20; NO 3; PP. 77-90; BIBL. 3 REF.Article

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

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

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