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

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

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 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

SIMULATION NUMERIQUE DE L'ECOULEMENT HYPERSONIQUE D'UN GAZ VISQUEUX AUTOUR D'UNE SPHEREBOBROV EM; KOLESNIKOV AF.1982; CISL. METODY MEH. SPLOS. SREDY; ISSN 505374; SUN; DA. 1982; VOL. 13; NO 1; PP. 16-20; BIBL. 8 REF.Article

COMPUTATION OF THREE-DIMENSIONAL VISCOUS FLOW OVER BLUNT LIFTING BODIES AT HIGH ANGLE OF ATTACKSZEMA KY; LEWIS CH.1981; THERMOPHYSICS CONFERENCE. 16/1981-06-23/PALO ALTO CA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 10 P.; BIBL. 18 REF.Conference Paper

INJECTION SLOT LOCATION FOR BOUNDARY LAYER CONTROL IN SHOCK-INDUCED SEPARATIONWISWANATH PR; SANKARAN L; NARASIMHA R et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1168; 9 P.; BIBL. 15 REF.Conference Paper

ECOULEMENT DANS UNE COUCHE DE CHOC DEVANT UN OBSTACLE PERPENDICULAIRE A L'AXE D'UN JET SUPERSONIQUE EN EXPANSION INCOMPLETESOKOLOV EI.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 4; PP. 51-58; BIBL. 12 REF.Article

FREE JET EXPANSION IN A RAPIDLY ROTATING GASMIKAMI H.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 4; PP. 471-473; BIBL. 13 REF.Article

COUCHE DE CHOC LIMITE EN AERODYNAMIQUE HYPERSONIQUEBARANTSEV RG.1977; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1977; NO 13; PP. 119-125; ABS. ANGL.; BIBL. 7 REF.Article

THE OCCURRENCE OF STAGNATION BUBBLES IN SUPERSONIC JET IMPINGEMENT FLOWS.KALGHATIGI GT; HUNT BL.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 3; PP. 169-185; BIBL. 1 P. 1/2Article

MOUVEMENT D'UNE COUCHE DE CHOC GAZEUSE AVEC UNE FRONTIERE LIBRE DANS LES CONDITIONS NON ADIABATIQUESCHEKMAREV SF.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 3; PP. 152-154; BIBL. 6 REF.Article

HYPERSONIC VISCOUS SHOCK-LAYER FLOW OVER A HIGHLY COOLED SPHERE.WASKIEWICZ JD; MURRAY AL; LEWIS CH et al.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 2; PP. 189-192; BIBL. 5 REF.Article

NON-EQUILIBRIUM BETWEEN ELECTRONS AND FIELDS IN A GAS BREAKDOWN IONISING WAVE. I: MACROSCOPIC MODELABBAS I; BAYLE P.1981; J. PHYS. D; ISSN 0022-3727; GBR; DA. 1981; VOL. 14; NO 4; PP. 649-660; BIBL. 17 REF.Article

A TWO-LAYER MODEL FOR COUPLED THREE-DIMENSIONAL VISCOUS AND INVISCID FLOW CALCULATIONSLIN TC; RUBIN SG; WIDHOPF GF et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 13 P.; BIBL. 43 REF.Conference Paper

APPLICATION OF AN IMPLICIT TECHNIQUE TO THE SHOCK-LAYER FLOW AROUND GENERAL BODIESLI CP.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 13 P.; BIBL. 21 REF.Conference Paper

ETUDE DE L'ABSORPTION D'UN RAYONNEMENT SELECTIF DANS UNE COUCHE-LIMITEKONDRANIN TV; KUZ'MINSKIJ IN.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 5; PP. 71-77; BIBL. 7 REF.Article

METHODS FOR PREDICTING RADIATION COUPLED FLOW FIELDS ABOUT PLANETARY ENTRY PROBES.NICOLET WE; WATERLAND LR; KENDALL RM et al.1977; IN: AM. INST. AERONAUT. ASTRONAUT. THERMOPHYS. CONF. 12; ALBUQUERQUE, N. MEX.; 1977; NEW YORK; AIAA; DA. 1977; VOL. 726; PP. (8P.); BIBL. 23 REF.Conference Paper

TURBULENT VISCOUS-SHOCK-LAYER SOLUTIONS WITH STRONG VORTICITY INTERACTION.ANDERSON EC; MOSS JN; SUTTON K et al.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 1; PP. 32-37; BIBL. 29 REF.Article

VISCOUS HYPERSONIC FLOW PAST BLUNTED CONES AT SMALL ANGLES OF ATTACK.AJAY KUMAR; GRAVES RA JR.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 8; PP. 1061-1062; BIBL. 8 REF.Article

INVISCID SUPERSONIC/HYPERSONIC BODY FLOWFIELD AND AERODYNAMICS FROM SHOCK-CAPTURING TECHNIQUE CALCULATIONS.CHAUSSEE DS; KUTLER P; HOLTZ T et al.1976; J. SPACEER. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 6; PP. 325-331; BIBL. 7 REF.Article

MODIFIED THIN SHOCK LAYER METHOD FOR SUPERSONIC FLOW PAST AN OSCILLATING CONE.HUI WH; MAHOOD GE.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 8; PP. 481-487; BIBL. 25 REF.Article