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Results 1 to 25 of 1063

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RESPONSE OF A CYLINDRICAL SHELL IN SUPERSONIC FLOW TO A SHOCK LOAD.DZYGADLO Z; NOWOTARSKI I; OLEJNIK A et al.1976; J. TECH. PHYS.; POLAND; DA. 1976; VOL. 17; NO 3; PP. 279-293; ABS. POL. RUSSE; BIBL. 9 REF.Article

ETUDE EXPERIMENTALE DES JETS CIRCULAIRES SONIQUES ET SUPERSONIQUESKOVAL MA; SHVETS AI.1979; P.M.T.F.; SUN; DA. 1979; NO 4; PP. 83-89; BIBL. 4 REF.Article

AN EXTENSION OF THE MOTT-SMITH METHOD FOR SHOCK WAVESBAQUERO R.1978; BOL. INST. TONANTZINTLA; MEX; DA. 1978; VOL. 2; NO 4; PP. 327-334; ABS. SPA; BIBL. 11 REF.Article

STATISTICAL ANALYSIS OF THE VIBRATION RESPONSE OF EXTERNAL AIRCRAFT STORES.HADAN G; ESHEL R.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 86-93; BIBL. 7 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper

SUPERSONIC FLOW DEVELOPMENT IN SLOTTED WIND TUNNELSRAMASWAMY MA; CORNETTE ES.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 6; PP. 805-811; BIBL. 10 REF.Article

PERFORMANCE OF CONICAL DIFFUSERS UP TO THE CHOKING CONDITIONMARKLAND E; NORTH P.1979; CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 2; PP. 703-714; BIBL. 7 REF.Conference Paper

DIRECTIVITY AND MACH NUMBER DEPENDENCE OF THE SOUND RADIATED FROM TURBULENT JETSCHANDRAKER AL; MUNJAL ML.1978; INDIAN J. TECHNOL.; IND; DA. 1978; VOL. 16; NO 1; PP. 18-24; BIBL. 17 REF.Article

OVERSHOOTS IN PLANETARY BOW SHOCKSRUSSELL CT; HOPPE MM; LIVESEY WA et al.1982; NATURE (LOND.); ISSN 0028-0836; GBR; DA. 1982; VOL. 296; NO 5852; PP. 45-48; BIBL. 11 REF.Article

IMPROVING THE MACH NUMBER CAPABILITIES OF ARC DRIVER SHOCK TUBESJOHNSON JA III; SANTIAGO J; LIN I et al.1980; REV. SCI. INSTRUM.; ISSN 0034-6748; USA; DA. 1980; VOL. 51; NO 10; PP. 1430-1431; BIBL. 8 REF.Article

SUR LA DEGENERESCENCE D'UN ECOULEMENT SUPERSONIQUE DANS LE CAS D'INTERACTION DES ONDES CENTREES DE COMPRESSION ET DE RAREFACTIONRYLOV AI.1979; PRIKL. MAT. MEKH.; SUN; DA. 1979; VOL. 43; NO 1; PP. 45-50; BIBL. 4 REF.Article

EFFECT OF ANGLE OF ATTACK AND MACH NUMBER ON SLENDER-WING UNSTEADY AERODYNAMICSERICSSON LE; REDING P.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 6; PP. 358-365; BIBL. 42 REF.Article

MACH NUMBER AND TEMPERATURE EFFECTS ON JETSLAU JC.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1152; 9 P.; BIBL. 14 REF.Conference Paper

SURFACE ROUGHNESS EFFECTS ON A MACH 6 TURBULENT BOUNDARY LAYERBERG DE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1159; 8 P.; BIBL. 17 REF.Conference Paper

MACH NUMBER DEPENDENCE OF LAMINAR NEAR-WAKE TRANSITION FOR SLENDER CONES.LEGNER HH; FINSON ML.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 417-419; BIBL. 16 REF.Article

Rigorous derivation of the anelastic approximationMASMOUDI, Nader.Journal de mathématiques pures et appliquées. 2007, Vol 88, Num 3, pp 230-240, issn 0021-7824, 11 p.Article

EVOLUTION D'ONDES ACOUSTIQUES DANS UNE ENCEINTE ET CONCEPT D'INCOMPRESSIBILITEZYTOUNIAN H; GUIRAUD JP.1981; REV. ACOUST.; ISSN 0557-7713; FRA; DA. 1981; VOL. 14; NO 58; PP. 143; ABS. ENG; BIBL. 1 REF.Conference Paper

COMPRESSIBILITY EFFECTS IN TURBULENT SHEAR LAYERSBOGDANOFF DW.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 6; PP. 926-927; BIBL. 11 REF.Article

EFFECTS OF MACH NUMBER ON THE DEVELOPMENT OF SUBSONIC RECTANGULAR JETHSIA Y; KROTHAPALLI A; BAGANOFF D et al.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 176-177; BIBL. 2 REF.Article

A NEW SPECIFIC POINT ON THE SHOCK POLARHIDA K.1982; JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN; ISSN 0031-9015; JPN; DA. 1982; VOL. 51; NO 4; PP. 1320-1323; BIBL. 7 REF.Article

PSEUDO-SHOCK WAVES IN A DIVERGENT CHANNELIKUI T; MATSUO K; MOCHIZUKI H et al.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 175; PP. 20-25; BIBL. 8 REF.Article

EXPERIMENTAL RESULTS OF LARGE-SCALE STRUCTURES IN JET FLOWS AND THEIR RELATION TO JET NOISE PRODUCTIONSAROHIA V; MASSIER PF.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 8; PP. 831-835; BIBL. 16 REF.Article

ECOULEMENTS GAZEUX PLANS, AVEC UN FAIBLE APPORT D'ENERGIEKOGAN MN; KUCHEROV AN; MIKHAJLOV VV et al.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 5; PP. 95-102; BIBL. 18 REF.Article

ACTIVE AND PASSIVE TRIPPING OF FRUSTUM TRANSITION AT MACH NUMBERS OF 8 AND 10THYSON N; TODISCO A; REEVES B et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1128; 17 P.; BIBL. 12 REF.Conference Paper

UTILISATION D'UNE COURBE UNIQUE DE CORRECTIONS POUR LES INDICATIONS DU TUBE DE PITOT DANS UN FLUX SUPERSONIQUE RAREFIELYSENKO EV.1976; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1976; NO 3; PP. 40-44; BIBL. 5 REF.Article

Low Mach number limit of the compressible magnetohydrodynamic equations with zero thermal conductivity coefficientJISHAN FAN; HONGJUN GAO; BOLING GUO et al.Mathematical methods in the applied sciences. 2011, Vol 34, Num 17, pp 2181-2188, issn 0170-4214, 8 p.Article

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