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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

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

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

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

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

PROCEEDINGS OF THE SECOND INTERNATIONAL SYMPOSIUM ON THE AERODYNAMICS AND VENTILATION OF VEHICLE TUNNELS. = RAPPORTS DU DEUXIEME CONGRES INTERNATIONAL SUR LES PROBLEMES D'AERODYNAMIQUE ET DE VENTILATION DES TUNNELS.1976; ; GBR; CRANFIELD: BRITISH HYDROMECH. RES. ASSOC.; DA. 1976; 810 P.; 29 CM; ISBN 0900983-51-5Conference Proceedings

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

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

EMPIRICAL ESTIMATES OF GUST LOADS ON FINITE WINGSPATEL MH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 12; PP. 1602-1604; BIBL. 7 REF.Article

A WIND TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF FORWARD SWEPT WINGSWEEKS TM; UHUAD GC; LARGE R et al.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 15 P.Conference Paper

PARTICULAR PROBLEMS OF DATA ACQUISITION AND ANALYSIS.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 210; PP. (20P.); BIBL. DISSEM.; (NUMER. METHODS WINDTUNNEL TEST. FLUID DYN. PANEL SPEC. MEET.; RHODE-ST-GENESE, BELG.; 1976)Conference Paper

INVESTIGATION OF A SIDE FORCE DUE TO ABLATIONRAGSDALE WC; HORANOFF EV.1978; A.I.A.A. J. NEW YORK; USA; DA. 1978; VOL. 16; NO 9; PP. 1010-1011; BIBL. 2 REF.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

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

UEBERLEGUNGEN ZUM PROBLEM DER INSTATIONAEREN STROEMUNG BEI EINER ZUGFAHRT DURCH EINEN TUNNEL. = REFLEXIONS SUR LE PROBLEME DU FLUX NON STATIONNAIRE LORS DU PASSAGE D'UN TRAIN DANS UN TUNNELGLUECK H.1976; ARCH. EISENBAHNTECH.; DTSCH.; DA. 1976; NO 31; PP. 77-81; ABS. ANGL. FR. ESP.; BIBL. 10 REF.Article

RESEARCH PROGRAMME AND MEASUREMENT TECHNIQUES IN THE WATER TOWING TANK OF DFVLR IN GOETTINGENBIPPES H; MAIER A.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. 53-60; BIBL. 8 REF.Conference Paper

DRUCKAENDERUNGEN BEIM EINTRITT EINES HOCHGESCHWINDIGKEITSZUGES IN EINEN TUNNEL = MODIFICATIONS DE LA PRESSION LORS DE L'ENTREE D'UN TRAIN A GRANDE VITESSE DANS UN TUNNELSELLMANN M; SPURK JH.1981; ING.-ARCH.; ISSN 0020-1154; DEU; DA. 1981; VOL. 50; NO 5; PP. 339-351; ABS. ENG; BIBL. 6 REF.Article

THE REDUCTION OF PRESSURE TRANSIENTS IN RAILWAYS TUNNELS.VARDY AE.1977; IN: THERMODYN. FLUID MECH. CONV. 6; DURHAM; 1976; LONDON; MECHANICAL ENGINEERING PUBL.; DA. 1977; PP. 195-200; BIBL. 6 REF.Conference Paper

INTERNATIONAL SYMPOSIUM ON THE AERODYNAMICS AND VENTILATION OF VEHICLE TUNNELS. 2. PROCEEDINGS; CAMBRIDGE; 1976.1976; CRANFIELD, ENGL.; BR. HYDROMECH. RES. ASSOC.; DA. 1976; PP. (700P.); BIBL. DISSEM.; ISBN 0900983515Conference Proceedings

LOW REYNOLDS NUMBER AERODYNAMIC CHARACTERISTICS OF LOW-DRAG NACA 63-208 AIRFOILNAGAMATSU HT; CUCHE DE.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 10; PP. 833-837; BIBL. 15 REF.Article

DREIKOMPONENTENMESSUNGEN AN EINEM FLUGKOERPERRUMPF MIT VERSCHIEDENEN HECKKONFIGURATIONEN IM UNTERSCHALL- UND TRANSSCHALLBEREICH = MESURE DE LA PORTANCE, DE LA TRAINEE ET DU MOMENT DE TANGAGE SUR UN MISSILE AVEC DIVERSES CONFIGURATIONS DE LA PARTIE ARRIERE POUR DES VITESSES SUBSONIQUES ET TRANSSONIQUESTANNER M.1979; D.F.V.L.R.-FORSCH.-BER.; DEU; DA. 1979; VOL. 79; NO 15; 85 P.; ABS. ENG; BIBL. 7 REF.Serial Issue

SUPPRESSEUR DE FLOTTEMENT EN TRANSSONIQUEDESTUYNDER R.1978; RECH. AEROSPAT.; FRA; DA. 1978; NO 3; PP. 117-123; ABS. ENG; BIBL. 3 REF.Article

CONSIDERATIONS ON WING STORES FLUTTER: ASYMMETRY, FLUTTER SUPPRESSION1978; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1978; AGARD-R-668; 37 P.; 30 CM; BIBL. DISSEM.; ISBN 92-835-1290-1Report

WIND TUNNEL INVESTIGATION OF THE TRANSONIC AERODYNAMIC CHARACTERISTICS OF FORWARD SWEPT WINGSUHUAD GC; WEEKS TM; LARGE R et al.1983; JOURNAL OF AIRCRAFT; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 3; PP. 195-202; BIBL. 3 REF.Article

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