THE APPLICATION OF A LIFTING-SURFACE METHOD TO LARGE, STEADY OR OSCILLATING MODELS IN SUBSONIC, CLOSED, OPEN OR SLOTTED WIND TUNNELS.STREATHER RA.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 1; PP. 41-55; BIBL. 9 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

USE OF SLOTTED WALLS TO REDUCE WIND-TUNNEL BOUNDARY CORRECTIONS IN SUBSONIC FLOW.PARKER AG.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1771-1772; BIBL. 9 REF.Article

INFLUENCIA DA RUGOSIDADE SUPERFICIAL NOS ESCOMMENTOS EXTERNOS. = INFLUENCE DE LA RUGOSITE SUPERFICIELLE DANS LES ECOULEMENTS EXTERNESMAGALHAES MARTINS FERREIRA S.1974; REV. BRAS. TECNOL.; BRAS.; DA. 1974; VOL. 5; NO 3-4; PP. 131-134; ABS. ANGL.; BIBL. 2 REF.Article

DIE VERDRAENGUNGSKORREKTUREN IN UNTERSCHALLWINDKANAELEN BEI SPERRIGEN MODELLEN AND MIT BODENSIMULATION. = CORRECTIONS DE DEPLACEMENT DANS LES SOUFFLERIES SUBSONIQUES DANS LE CAS DE MAQUETTES VOLUMINEUSES ET DE SIMULATION AU SOLSCHULZ G.1974; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 46; PP. 1-119; ABS. ANGL.; BIBL. 4 REF.Article

INTEGRAL EQUATION METHOD FOR SUBSONIC FLOW PAST AIRFOILS IN VENTILATED WIND TUNNELS.MOKRY M.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 1; PP. 47-53; BIBL. 29 REF.Article

INSTATIONAERE DRUCKVERTEILUNGEN AN SCHWINGENDEN SCHLANKEN FLUEGEL-RUMPF-KOMBINATIONEN. VERGLEICH ZWISCHEN THEORIE UND MESSUNG. = DISTRIBUTIONS DES PRESSIONS INSTATIONNAIRES SUR LES CONFIGURATIONS AILE-FUSELAGE ELANCEES EN OSCILLATION. COMPARAISON DE LA THEORIE ET DES MESURESTRIEBSTEIN H; WAGENER J.1974; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 47; PP. 1-75; ABS. ANGL.; BIBL. 1 P. 1/2Article

WIND-TUNNEL BALANCE BASED ON PIEZOELECTRIC QUARTZ FORCE TRANSDUCERSBRIDEL G; THOMANN H.1980; J. AVICR.; USA; DA. 1980; VOL. 17; NO 5; PP. 374-376; BIBL. 2 REF.Article

BEMERKUNGEN ZUR AUSLEGUNG EINES UNTERSCHALL-FREISTRAHLWINDKANALS = REMARQUES SUR LA CONCEPTION D'UNE SOUFFLERIE SUBSONIQUE A JETS LIBRESVAGT JD.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 5; PP. 159-162; ABS. ANGL. FR.; BIBL. 8 REF.Serial Issue

NUMERICAL SIMULATION OF THE WIND TUNNEL ENVIRONMENT BY A PANEL METHODLEE KD.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 4; PP. 470-475; BIBL. 15 REF.Article

SIX-COMPONENT STRAIN-GAGE BALANCES FOR LARGE WIND TUNNELSDUBOIS M.1981; EXP. MECH.; ISSN 0014-4851; USA; DA. 1981; VOL. 21; NO 11; PP. 401-407; BIBL. 25 REF.Article

ETUDE THEORIQUE ET EXPERIMENTALE DES ECOULEMENTS PULSES EN CANALISATION CIRCULAIRE.THOMAS JM.1974; AO-CNRS-11162; FR.; DA. 1974; PP. 1-184; H.T. 86; BIBL. 5 P. 1/2; (THESE DOCT. SCI.; ORLEANS)Thesis

EFFECTS OF SIDEWALL BOUNDARY LAYERS IN TWO-DIMENSIONAL SUBSONIC AND TRANSONIC WIND TUNNELSSEWALL WG.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 9; PP. 1253-1256; BIBL. 10 REF.Article

DESIGN AND DEVELOPMENT OF THE UNITED AIRCRAFT RESEARCH LABORATORIES ACOUSTIC RESEARCH TUNNELPATTERSON RW; VOGT PG; FOLEY WM et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-13; BIBL. 11 REF.Conference Paper

NUMERICAL SIMULATION OF THE WIND TUNNEL ENVIRONMENT BY A PANEL METHODLEE KD.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 24-30; BIBL. 13 REF.Conference Paper

ETUDE SUR MAQUETTE DE DIFFERENTES CONFIGURATIONS DE JET TRAVERSANT UNE CAVITE: APPLICATION A LA SOUFFLERIE CEPRA 19 DU CEPRREBUFFET P; GUEDEL A.1982; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1982; VOL. 206; NO 1; PP. 11-22; ABS. ENG; BIBL. 8 REF.Article

DISTRIBUICAO DE PRESSAO PERIFERICA EM CONDENSACAO FORCADA SOBRE CILINDRO CIRCULAR. = DISTRIBUTION DES PRESSIONS LORS DE LA CONDENSATION FORCEE AUTOUR D'UN CYLINDRE CIRCULAIREMARTINS FERREIRA SM.1974; REV. BRAS. TECNOL.; BRAS.; DA. 1974; VOL. 5; NO 1-2; PP. 83-85; ABS. ANGL.; BIBL. 8 REF.Article

ELEKTRISCHE AUSRUESTUNG EINES KLIMAWINDKANALS IN EINEM AUTOMOBILWERK. = EQUIPEMENT ELECTRIQUE D'UN TUNNEL AERODYNAMIQUE DANS UNE USINE D'AUTOMOBILESWEYLAND W.1977; B.B.C. NACHR.; DTSCH.; DA. 1977; VOL. 59; NO 10; PP. 399-407Article

Simulation of honeycomb-screen combinations for turbulence management in a subsonic wind tunnelKULKARNI, Vinayak; SAHOO, Niranjan; CHAVAN, Sandip D et al.Journal of wind engineering and industrial aerodynamics. 2011, Vol 99, Num 1, pp 37-45, issn 0167-6105, 9 p.Article

Flow structure around two finite circular cylinders located in an atmospheric boundary layer: side-by-side arrangementPARK, C. W; LEE, S. J.Journal of fluids and structures. 2003, Vol 17, Num 8, pp 1043-1058, issn 0889-9746, 16 p.Article

The aeroelastic response of a wing section with a structural freeplay nonlinearity : An experimental investigationMARSDEN, C. C; PRICE, S. J.Journal of fluids and structures. 2005, Vol 21, Num 3, pp 257-276, issn 0889-9746, 20 p.Conference Paper

Dynamic aero-structural response of an elastic wing modelKÄMPCHEN, M; DAFNIS, A; REIMERDES, H.-G et al.Journal of fluids and structures. 2003, Vol 18, Num 1, pp 63-77, issn 0889-9746, 15 p.Article

Effects of free-end corner shape on flow structure around a finite cylinderPARKA, C. W; LEE, S. J.Journal of fluids and structures. 2004, Vol 19, Num 2, pp 141-158, issn 0889-9746, 18 p.Article