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Results 1 to 25 of 302

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LAMINAR AND TURBULENT VISCOUS SHOCK LAYER FLOW IN THE SYMMETRY PLANES OF BODIES AT ANGLE OF ATTACK.EATON RR; LARSON DE.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 599; PP. 1-11; BIBL. 13 REF.Conference Paper

RADIATION-GAS DYNAMIC SHOCK LAYER COUPLING.ENGEL CD; FARMER RC.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1144-1146; BIBL. 10 REF.Article

ETUDE DE L'ACTION D'UNE INSUFFLATION SUR L'ECOULEMENT D'UNE COUCHE DE CHOC VISQUEUX HYPERSONIQUE PRES DE LA LIGNE D'ARRET D'UN CORPS EMOUSSEGERSHBEJN EH A; KOLESNIKOV AF.1980; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1980; NO 1; PP. 199-202; BIBL. 15 REF.Article

ENGINEERING APPROXIMATIONS FOR RADIATING NONEQUILIBRIUM SHOCK LAYERS.CARLSON LA.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 832-837; BIBL. 18 REF.Article

NONEQUILIBRIUM MERGED STAGNATION SHOCK LAYERS AT HYPERSONIC SPEEDS.AJAY KUMAR; JAIN AC.1975; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1975; VOL. 18; NO 10; PP. 1113-1118; ABS. FR. ALLEM. RUSSE; BIBL. 10 REF.Article

THREE-DIMENSIONAL HYPERSONIC LAMINAR, TRANSITIONAL, AND FOR TURBULENT SHOCK-LAYER FLOWSSZEMA KY; LEWIS CH.1982; J. SPACECR. ROCKETS; ISSN 0022-4650; USA; DA. 1982; VOL. 19; NO 1; PP. 88-89; BIBL. 8 REF.Article

HYPERSONIC VISCOUS STATIC STABILITY OF A SHARP 5-DEG CONE AT INCIDENCE.ADAMS JC JR; GRIFFITH BJ.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 8; PP. 1062-1068; BIBL. 21 REF.Article

DENSITY SURVEY IN THE HYPERSONIC VISCOUS SHOCK LAYER ON A SHARP FLAT PLATE.AVIDOR JM; LEDERMAN S.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 7; PP. 993-995; BIBL. 9 REF.Article

A STUDY OF IMPLICIT DIFFERENCE SCHEMES FOR INVISCID EQUATIONSSRIVASTAVA BN; WERLE MJ; DAVIS RT et al.1980; COMPUT. FLUIDS; ISSN 0045-7930; USA; DA. 1980; VOL. 8; NO 4; PP. 413-420; BIBL. 12 REF.Article

ETUDE DE LA COUCHE DE CHOC VISQUEUSE TRIDIMENSIONNELLE HYPERSONIQUE AU VOISINAGE DU POINT CRITIQUE, EN PRESENCE D'INSUFFLATION OU D'ASPIRATIONGERSHBEJN EH A; YUNITSKIJ SA.1979; PRIKL. MAT. MEKH.; SUN; DA. 1979; VOL. 43; NO 5; PP. 817-828; BIBL. 23 REF.Article

IMPLICIT SOLUTION FOR THE SHOCK-LAYER FLOW AROUND GENERAL BODIESLI CP.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 2; PP. 175-183; BIBL. 21 REF.Article

ON THE VALIDITY OF THE NAVIER-STOKES RELATION IN A SHOCK WAVE.ELLIOTT JP.1975; CANAD. J. PHYS.; CANADA; DA. 1975; VOL. 53; NO 6; PP. 583-586; ABS. FR.; BIBL. 11 REF.Article

ETUDE EXPERIMENTALE DE QUELQUES CARACTERISTIQUES D'UN ECOULEMENT SUPERSONIQUE AUTOUR DES AILES EN FORME DE VZUBIN MA; OSTAPENKO NA.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; VOL. 2; NO 4; PP. 130-135; BIBL. 11 REF.Article

FLOW REGIMES OVER DELTA WINGS AT SUPERSONIC AND HYPERSONIC SPEEDS.SQUIRE LC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 1; PP. 1-14; BIBL. 16 REF.Article

SIMPLE TECHNIQUE FOR PREDICTING TYPE III AND IV SHOCK INTERFERENCE.BRAMLETTE TT.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1151-1152; BIBL. 8 REF.Article

HYPERSONIC FLOW OVER CONICAL WING-BODY COMBINATIONSMILLIER R.1978; AERONAUT. QUART.; GBR; DA. 1978; VOL. 29; NO 4; PP. 285-304; BIBL. 13 REF.Article

APPROXIMATION DU SECOND ORDRE DANS LA THEORIE DE L'AILE MINCE FINIE PLACEE DANS UN ECOULEMENT GAZEUX HYPERSONIQUEBOGATKO VI; GRIB AA; KOLTON GA et al.1979; VEST. LENINGRAD. UNIV.; SUN; DA. 1979; NO 1; PP. 88-95; ABS. ENG; BIBL. 8 REF.Article

HYPERSONIC IONIZING AIR VISCOUS SHOCK-LAYER FLOWS OVER SPHERE CONES.MINER EW; LEWIS CH.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 1; PP. 80-88; BIBL. 25 REF.Article

ECOULEMENT AUTOUR DES CONES EMOUSSES PENETRANT DANS UNE ATMOSPHERE D'AZOTE ET DE GAZ CARBONIQUEGOLOVACHEV YU P; POPOV FD.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 175-178; BIBL. 7 REF.Article

EINFLUSS DER DIFFUSION UND THERMODIFFUSION AUF STOSSGRENZSCHICHTEN IN SAUERSTOFF. = INFLUENCE DE LA DIFFUSION ET DE LA THERMODIFFUSION SUR LES COUCHES LIMITES DE CHOC EN OXYGENEMOHAMMED ALI MOVAHED; GROENIG H.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 2; PP. 70-75; ABS. ANGL. FR.; BIBL. 24 REF.Article

INVISCID HYPERSONIC FLOW AROUND A SEMICONE BODY. = ECOULEMENT HYPERSONIQUE NON VISQUEUX AUTOUR D'UN CORPS SEMI-CONIQUEKIMURA T; TSUTAHARA M.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1349-1353; BIBL. 7 REF.Article

ECOULEMENT D'UN FLUX ELECTROGAZODYNAMIQUE SUPERSONIQUE SUR DES CORPS AVEC FORMATION D'UNE COUCHE GAZEUSE DE CHOC ELECTROCONDUCTRICEVARENTSOV OK; VATAZHIN AB; GRABOVSKIJ VI et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 6; PP. 135-146; BIBL. 8 REF.Article

THEOREMES D'EXISTENCE DE LA SOLUTION POUR UN PROBLEME AUX LIMITES AUTOMODELE D'UNE COUCHE DE CHOC HYPERSONIQUE VISQUEUSETITOV OV.1979; ZH. VYCHISLIT. MAT. MAT. FIZ.; SUN; DA. 1979; VOL. 19; NO 3; PP. 701-707; BIBL. 3 REF.Article

HYPERSONIC FLOW WITH ATTACHED SHOCK WAVES OVER PLANE DELTA WINGS.WOODS BA; MCINTOSH CBG.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 79; NO 2; PP. 361-377; BIBL. 17 REF.Article

LAMINAR VISCOUS SHOCK LAYER ON A BLUNT BICONIC AT INCIDENCE.MAYNE AW JR.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 11; PP. 1541-1542; BIBL. 6 REF.Article

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