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CALCUL DE L'ECOULEMENT GAZEUX DANS UNE GRILLE DROITE DE PROFILS QUELCONQUESZAJTSEV VP.1978; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; SUN; DA. 1978; NO 3; PP. 112-117; BIBL. 13 REF.Article

ETUDE DES DIFFUSEURS RADIAUX AVEC ECOULEMENT TOURBILLONNAIREVOLOV VT; SHAKHOV VG.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1978; VOL. 21; NO 3; PP. 148-150; BIBL. 3 REF.Article

AERODYNAMICS OF A FINITE ASPECT RATIO JET FLAP AT LOW FLIGHT SPEEDS.ADDESSIO FL; SKIFSTAD JG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 936-943; BIBL. 16 REF.Article

THE PRESSURE DISTRIBUTION ON THE SURFACE OF AN ELLIPSOID IN INVISCID FLOWBAND E GU; PAYNE PR.1980; AERONAUT. QUART.; GBR; DA. 1980; VOL. 31; NO 1; PP. 70-84; BIBL. 8 REF.Article

CALCUL DE L'ECOULEMENT TURBULENT DU GAZ DANS UN DIFFUSEUR AXIAL-RADIAL EN PRESENCE DE CONTRE-COURANTSZHUKOVSKI MI; KARYAKIN YU E.1978; ENERGO-MASHINOSTR.; SUN; DA. 1978; NO 8; PP. 7-10; BIBL. 8 REF.Article

ONDES DE RIEMANN DANS UN LIQUIDE CONDUCTEURZHUKOV VI.1976; SOLNECH. DANNYE, BJULL.; S.S.S.R.; DA. 1976; NO 5; PP. 54-56; ABS. ANGL.Article

TRANSONIC FLOW PAST AXISYMMETRIC AND NONAXISYMMETRIC BOATTAIL PROJECTILESSTAHARA SS; ELLIOTT JP; SPREITER JR et al.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1329-1337; BIBL. 13 REF.Article

COEFFICIENT MATRICES FOR IMPLICIT FINITE DIFFERENCE SOLUTION OF THE INVISCID FLUID CONSERVATION LOW EQUATIONS.STEGER JL.1978; COMPUTER METHODS APPL. MECH. ENGNG; NETHERL.; DA. 1978; VOL. 13; NO 2; PP. 175-188; BIBL. 22 REF.Article

INVISCID FLOWFIELD CALCULATIONS FOR RE-ENTRY VEHICLES WITH CONTROL SURFACES.SOLOMON JM; CIMENT M; FERGUSON RE et al.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 1742-1749; BIBL. 20 REF.Article

ON THE FLOW IN A CENTRIFUGAL IMPELLER (1ST REPORT, SUBSONIC COMPRESSIBLE FLOW).MURATA S; OGAWA T; GOTOH M et al.1977; BULL. J.S.M.E.; JAP.; DA. 1977; VOL. 20; NO 140; PP. 183-190; BIBL. 12 REF.Article

ON THE STEADY MOTION OF JETS WITH ELLIPTICAL SECTIONS.GREEN AE.1977; ACTA MECH.; AUTR.; DA. 1977; VOL. 26; NO 1; PP. 171-177; ABS. ALLEM.; BIBL. 10 REF.Article

AMPLIFICATION OF HELICAL DISTURBANCES IN A ROUND JET.LOPEZ JL; HURZWEG UH.1977; PHYS. OF FLUIDS; U.S.A.; DA. 1977; VOL. 20; NO 5; PP. 860-861; BIBL. 4 REF.Article

NUMERICAL INVESTIGATION OF FLOWFIELD ABOUT A SERIES OF INDENTED NOSETIPSHSIEH T.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 10 P.; H.T. 1; BIBL. 16 REF.Conference Paper

FLOW OVER A WING WITH AN ATTACHED FREE VORTEX.SAFFMAN PG; SHEFFIELD JJ.1977; STUD. APPL. MATH.; U.S.A.; DA. 1977; VOL. 57; NO 2; PP. 107-117; BIBL. 7 REF.Article

ECOULEMENT SUPERSONIQUE AUTOUR DES AILES A BOUTS POINTUSVOSKRESENSKIJ GP; IL'INA AS; TATARENCHIK VS et al.1977; P.M.T.F.; S.S.S.R.; DA. 1977; NO 6; PP. 35-42; BIBL. 4 REF.Article

ECOULEMENT SUPERSONIQUE AUTOUR D'UN CONE MINCE A BEC ASYMETRIQUEVISHNEVETSKIJ SL; IVANOV MA.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 1; PP. 144-149; BIBL. 9 REF.Article

COMPUTATION OF INVISCID TRANSONIC INTERNAL FLOWGIESE U.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 217-223; BIBL. 9 REF.Conference Paper

NUMERICAL EXPERIMENTS ON THE LEADING-EDGE FLOWFIELDZANNETTI L; MORETTI G.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1668-1673; BIBL. 11 REF.Article

NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST WINGS OF ARBITRARY FORM WITH A DETACHED SHOCK WAVEVOSKRESENSKY GP.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 513-518; BIBL. 2 REF.Conference Paper

ON THE JET CURTAIN OVER WATERTSENIK DS.1982; J. SHIP. RES.; ISSN 0022-4502; USA; DA. 1982; VOL. 26; NO 2; PP. 77-88; BIBL. 1 P.Article

SIMULTANEOUS SOLUTION OF THE INVISCID FLOW AND BOUNDARY LAYERS FOR COMPRESSOR CASCADESMOSES HL; THOMASON SB; JONES RR III et al.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1466-1468; BIBL. 5 REF.Article

UN THEOREME D'EXISTENCE ET D'UNICITE CONCERNANT LES ECOULEMENTS COMPRESSIBLES AUTOUR D'UN PROFIL A POINTECIAVALDINI JF; POGU M; TOURNEMINE G et al.1982; REV. ROUM. MATH. PURES APPL.; ISSN 0035-3965; ROM; DA. 1982; VOL. 27; NO 3; PP. 291-298; ABS. ENG; BIBL. 8 REF.Article

COMPARISON OF FIVE MODELS OF SPHERICAL BUBBLE RESPONSE IN AN INVISCID COMPRESSIBLE LIQUIDLASTMAN GJ; WENTZELL RA.1981; J. ACOUST. SOC. AM.; ISSN 0001-4966; USA; DA. 1981; VOL. 69; NO 3; PP. 638-642; BIBL. 19 REF.Article

CALCUL DE LA FRONTIERE D'UN JET NON VISQUEUX SUPERSONIQUE S'ECOULANT DANS UN ESPACE NOYE OU DANS UN FLUX SUPERSONIQUE COCOURANTBELOTSERKOVETS IS; TIMOSHENKO VI.1981; INZ.-FIZ. Z.; ISSN 0021-0285; BYS; DA. 1981; VOL. 40; NO 2; PP. 197-203; ABS. ENG; BIBL. 11 REF.Article

PROPAGACAO DE ONDAS DE ACELERACAO EM MISTURAS TRANSVERSALMENTE ISOTROPICAS = PROPAGATION D'ONDES D'ACCELERATION DANS DES MELANGES TRANSVERSALEMENT ISOTROPESKREMER GM; I SHIH LIU.1981; REV. BRAS. FIS.; ISSN 0374-4922; BRA; DA. 1981; VOL. 11; NO 3; PP. 543-558; BIBL. 6 REF.Article

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