kw.\*:("ECOULEMENT SUBSONIQUE")
Results 1 to 25 of 1519
Selection :
LA VEINE D'ESSAIS DE LA SOUFFLERIE SUBSONIQUE DE TOULOUSE (FRANCE).LAFITTE J.1976; ACIER STAHL STEEL; FR.; DA. 1976; VOL. 41; NO 4; PP. 141-145Article
SUBSONIC AERODYNAMICSDELAURIER JD; REID LD.1978; INST. AEROSPACE STUD., UNIV. TORONTO, ANNU. PROGR. REP.; CAN; DA. 1978; PP. 57-58; BIBL. 7 REF.Article
ETUDE DES ECOULEMENTS MIXTES TRIDIMENSIONNELS DANS LES TUYERES AVEC ENTREE ASYMETRIQUEDVORETSKIJ VM.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 167-169; BIBL. 9 REF.Article
SUBSONIC FLOW INTO A DOWNSTREAM FACING INLET.KEITH TG JR.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 251-252; BIBL. 1 REF.Article
OSCILLATIONS OF A WEDGE IN A FREE STREAM WITH PARTICULAR REFERENCE TO PARACHUTES.REDDY KR; ROBERTS BW.1975; APPL. SCI. RES.; NETHERL.; DA. 1975; VOL. 31; NO 4; PP. 279-308Article
THE GERMAN-DUTCH LOW SPEED WIND TUNNEL DNW.SEIDEL M; JAARSMA F.1978; AERONAUT. J.; G.B.; DA. 1978; VOL. 82; NO 808; PP. 167-173Article
ETUDE DE LA SOLLICITATION D'UN ECOULEMENT NON STATIONNAIRE ET NON UNIFORME SUIVANT LE POURTOUR SUR UNE GRILLE D'AUBES ANNULAIRE ACCELERATRICEGINZBURG SI; RABINOVICH GI; SUSLENNIKOV LA et al.1976; PROBL. PROCHN., U.S.S.R.; S.S.S.R.; DA. 1976; NO 3; PP. 33-37; BIBL. 7 REF.Article
EINBAU EINES STROEMUNGSGLEICHRICHTERS IN DEN UNTERSCHALLWINDKANAL. = MONTAGES D'UN REDRESSEUR D'ECOULEMENT DANS UNE SOUFFLERIE SUBSONIQUEZUDA E.1975; D.F.V.L.R.-NACHR.; DTSCH.; DA. 1975; NO 17; PP. 697-698Article
A COMPARISON OF TWO INTEGRAL EQUATION METHODS FOR HIGH SUBSONIC LIFTING FLOWS.NIXON D.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 1; PP. 56-58; BIBL. 2 REF.Article
EIN NUMERISCHES VERFAHREN ZUR BERECHNUNG DER INSTATIONAEREN AERODYNAMISCHEN DRUCKVERTEILUNG DER HARMONISCH SCHWINGENDEN TRAGFLAECHE MIT RUDER IN UNTERSCHALLSTROEMUNG. THEORIE UND ERGEBNISSE FUER IKOMPRESSIBLE STROEMUNG. I. = METHODE NUMERIQUE POUR CALCULER LA DISTRIBUTION DE PRESSION AERODYNAMIQUE NON STATIONNAIRE SUR UNE AILE EN OSCILLATIONS HARMONIQUES DANS UN ECOULEMENT SUBSONIQUE. THEORIE ET RESULTATS POUR UN FLUIDE INCOMPRESSIBLE (PARTIE I)GEISSLER W.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 37; PP. 1-91; ABS. ANGL.; BIBL. 7 REF.Article
ANALYSE DES CONDITIONS DE SORTIE DANS L'ECOULEMENT DANS UNE GRILLE D'AUBES PLANES, AVEC UN ECOULEMENT SUBSONIQUE A L'ENTREEKOZEL K; POLASEK J.1975; STROJN. CAS.; CESKOSL.; DA. 1975; VOL. 26; NO 5; PP. 532-539; ABS. RUSSE; BIBL. 5 REF.Article
PERFORMANCE CHARACTERISTICS OF AN 8-IN-DIA ASME NOZZLE OPERATING AT COMPRESSIBLE AND INCOMPRESSIBLE CONDITIONS.SMITH RE JR; MATZ RJ.1973; J. FLUIDS ENGNG; U.S.A.; DA. 1973; VOL. 95; NO 4; PP. 542-550; BIBL. 10 REF.Article
QUADRATURE FORMULAS FOR CHORDWISE INTEGRALS OF LIFTING SURFACE THEORIESANDO S; ICHIKAWA A.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 3; PP. 466-467; BIBL. 6 REF.Article
HIGH-FREQUENCY SUBSONIC FLOW PAST A PULSATING THIN AIRFOIL.PLOTKIN A.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 4; PP. 405-407; BIBL. 8 REF.Article
AERODYNAMIQUE SUBSONIQUE D'UN ECOULEMENT LIBRE AUTOUR D'UN CORPS ARBITRAIREKOVAL FF.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 5; PP. 416-420; ABS. ANGL. RUSSE; BIBL. 8 REF.Article
SUBSONIC AXISYMMETRIC NEAR-WAKE STUDIESMERZ RA; PAGE RH; PRZIREMBEL CEG et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 656-662; BIBL. 25 REF.Article
LOW-FREQUENCY APPROXIMATIONS IN UNSTEADY SMALL PERTURBATION SUBSONIC FLOWS.AMIET RK.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 75; NO 3; PP. 545-552; BIBL. 16 REF.Article
THE HODOGRAPH METHOD IN FLUID-DYNAMICS IN THE LIGHT OF VARIATIONAL INEQUALITIES.BREZIS H; STAMPACCHIA G.1976; ARCH. RATION. MECH. ANAL.; GERM.; DA. 1976; VOL. 61; NO 1; PP. 1-18; BIBL. 8 REF.Article
THE PRESSURE AT THE REATTACHEMENT POINT IN SUBSONIC TWO-DIMENSIONAL STEADY BASE FLOW.TANNER M.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 1; PP. 55-65; BIBL. 13 REF.Article
STEADY AND OSCILLATORY SUBSONIC AND SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATIONS.MORINO L; LEE TZONG CHEN; SUCIU EO et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 3; PP. 368-374; BIBL. 28 REF.Article
AERODYNAMIQUE DES VITESSES HYPOSONIQUES (ECOULEMENTS A PETITS NOMBRES DE MACH)ZEJTUNYAN R KH.1983; PMTF. ZURNAL PRIKLADNOJ MEHANIKI I TEHNICESKOJ FIZIKI; ISSN 0044-4626; SUN; DA. 1983; NO 2; PP. 53-61; BIBL. 27 REF.Article
DOUBLET LATTICE METHOD-SCHEMES FOR CPU TIME REDUCTIONSIMHA PRASAD DS; HOLLA VS.1980; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1980; VOL. 23; NO 1; PP. 59-65; BIBL. 4 REF.Article
A ONE-DIMENSIONAL ANALYSIS AND PERFORMANCE PREDICTION OF SUBSONIC RADIAL TURBINESHAMAJIMA M.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 186; PP. 2064-2070; BIBL. 14 REF.Article
LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 551; PP. 1-10; BIBL. 11 REF.Conference Paper
COMPUTER MODEL OF A FULLY DEPLOYED PARACHUTE.TORY C; AYRES R.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 675-679; BIBL. 5 REF.Article