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THE EFFECT OF NOSE BLUNTING ON THE WAVE DRAG OF OGIVE FOREBODIESPARTINGTON R; BAKER TJ.1982; AERONAUT. Q.; ISSN 0001-9259; GBR; DA. 1982; VOL. 33; NO 3; PP. 258-270; BIBL. 14 REF.Article

NONLINEARITY OF THE THREE-DIMENSIONAL FLOW PAST A FLAT BLUNT SHIPFERNANDEZ G.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 108; PP. 345-361; BIBL. 15 REF.Article

REAL-GAS EFFECTS ON THE AERODYNAMICS OF BLUNT CONES AS MEASURED IN A HYPERVELOCITY RANGEWELSH CJ; LAWRENCE WR; WATT RM et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 9 P.; BIBL. 12 REF.Conference Paper

TRAINEE NON VISQUEUSE HYPERSONIQUE DANS L'AIRPOLYANSKIJ AF; SKURIN LI.1977; UCHEN. ZAP. LENINGRAD. GOS. UNIV., MAT. NAUK; S.S.S.R.; DA. 1977; NO 55; PP. 64-71; BIBL. 6 REF.Article

VIBRATION AEROELASTIQUE DES CORPS EMAISSES EXCITEE PAR LE VENT1982; NONLINEAR VIBRATION PROBLEMS; ISSN 0044-1597; POL; DA. 1982; NO 20; PP. 17-45; ABS. POL/ENG; BIBL. 26 REF.Article

CALCULATION OF PRESSURES ON BODIES AT LOW ANGLES OF ATTACK IN SUPERSONIC FLOWDE JARNETTE FR; FORD CP.1980; J. SPACE ROCKETS; ISSN 0022-4650; USA; DA. 1980; VOL. 17; NO 6; PP. 529-536; BIBL. 11 REF.Article

SUPERCRITICAL FLOW PAST BLUNT BODIES IN SHALLOW WATERFORBES LK; SCHWARTZ LW.1981; Z. ANGEW. MATH. PHYS.; ISSN 0044-2275; CHE; DA. 1981; VOL. 32; NO 3; PP. 314-328; ABS. GER; BIBL. 14 REF.Article

TRANSFERT DE CHALEUR NON STATIONNAIRE PRES DU POINT D'ARRETSERGEEV VL.1981; INZ.-FIZ. Z.; ISSN 0021-0285; BYS; DA. 1981; VOL. 40; NO 2; PP. 218-224; ABS. ENG; BIBL. 8 REF.Article

ZONE DE DISCONTINUITE AVANT DANS UN ECOULEMENT AUTOUR D'UN CORPS EMOUSSE (MODELE DE CALCUL)BELOV IA; ZHIGALKO EF.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 2; PP. 184-187; BIBL. 8 REF.Article

COMPLETE SUPERSONIC FLOWFIELDS OVER BLUNT BODIES IN A GENERALIZED ORTHOGONAL COORDINATE SYSTEMGNOFFO PA.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 6; PP. 611-612; BIBL. 7 REF.Article

BLUNT-BODY TURBULENT BOUNDARY-LAYER PARAMETERS INCLUDING SHOCK SWALLOWING EFFECTSGRIFFITH BJ; MAJORS BM; ADAMS JC JR et al.1982; PROGR. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1982; VOL. 82; PP. 90-111; BIBL. 16 REF.Conference Paper

SIMILITUDE DES ECOULEMENTS HYPERSONIQUES D'UN GAZ RAREFIE AUTOUR DE CORPS EMOUSSESLARIN IN; RYKOV VA.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 2; PP. 130-135; BIBL. 9 REF.Article

UTILISATION DES SYSTEMES DE COORDONNEES CURVILIGNES NON ORTHOGONALES POUR LE CALCUL D'UN ECOULEMENT SUPERSONIQUE AUTOUR DE LA PARTIR AVANT DES CORPS EMOUSSES SOUS DE GRANDS ANGLES D'ATTAQUEPOGORELOV NV; SHEVELEV YU D.1981; CISL. METODY MEH. SPLOS. SREDY; ISSN 505374; SUN; DA. 1981; VOL. 12; NO 6; PP. 65-79; BIBL. 11 REF.Article

INJECTION FORTE DE GAZ A LA SURFACE D'UNE SPHERE EMOUSSEE DANS LE CAS D'ECOULEMENT SUPERSONIQUEANTONOV VA.1982; CISL. METODY MEH. SPLOS. SREDY; ISSN 505374; SUN; DA. 1982; VOL. 13; NO 1; PP. 3-10; BIBL. 16 REF.Article

STOKES FLOW PAST A SMOOTH CYLINDERDORREPAAL JM.1978; J. ENGNG MATH.; NLD; DA. 1978; VOL. 12; NO 2; PP. 177-185; BIBL. 9 REF.Article

DE L'INFLUENCE DES PHENOMENES PHYSICO-CHIMIQUES SUR LA FRICTION SUPERFICIELLE, DANS L'ECOULEMENT HYPERSONIQUE D'UN GAZ AUTOUR D'UN CORPS OBTUSGOLOVACHEV YU P; POPOV FD.1976; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1976; VOL. 31; NO 6; PP. 1126-1128; ABS. ANGL.; BIBL. 7 REF.Article

NUMERICAL SOLUTION OF SUPERSONIC VISCOUS FLOW OVER BLUNT DELTA WINGSTANNEHILL JC; VENKATAPATHY E; RAKICH JV et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 18 P.; BIBL. 22 REF.Conference Paper

ECOULEMENT SUR DES CORPS EMOUSSES ET POSSEDANT DES CONES ET DES ALVEOLESDAVYDOV YU M; KOROBITSYN GP; POSTNIKOV VG et al.1979; INZ.-FIZ. Z.; ISSN 0021-0285; BYS; DA. 1979; VOL. 37; NO 4; PP. 712-716; ABS. ENG; BIBL. 11 REF.Article

MHD WITH INERTIA: FLOW OVER BLUNT OBSTACLES IN CHANNELS.KAPILA AK; LUDFORD GSS.1977; INTERNATION. J. ENGNG SCI.; G.B.; DA. 1977; VOL. 15; NO 8; PP. 465-480; BIBL. 11 REF.Article

INTEGRAL MOMENTUM EQUATION FOR FLOWS WITH ENTROPY GRADIENTS ACROSS INVISCID STREAMLINES.ANDERSON A.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 983-985; BIBL. 1 REF.Article

AN EXPERIMENTAL STUDY OF PARTICLE INDUCED CONVECTIVE HEATING AUGMENTATION.HOLDEN MS; GUSTAFSON GQ; DURYEA GR et al.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 320; PP. 1-15; H.T. 23; BIBL. 8 REF.Conference Paper

EFFECTS OF THICK BOUNDARY LAYERS ON SUPERSONIC TURBULENT BASE HEAT TRANSFER.INOUE Y; PAGE RH.sdIN: CANCAM'77. CAN. CONGR. APPL. MECH. 6. PROC.; VANCOUVER, B.C.; 1977; S.L.; DA. S.D.; VOL. 2; PP. 567-568; BIBL. 5 REF.Conference Paper

HEAT TRANSFER IN THE VICINITY OF A STAGNATION POINT WITH STEP WISE VARIATIONS OF THE TEMPERATURE FLOWSERGEEV VL; STROGIJ AS.1981; INZ.-FIZ. Z.; ISSN 0021-0285; BYS; DA. 1981; VOL. 40; NO 6; PP. 970-974; ABS. ENG; BIBL. 8 REF.Article

A CONTRIBUTION TO THE COMPUTATION OF TRANSONIC SUPERSONIC FLOWS OVER BLUNT BODIESWEILAND C.1981; COMPUT. FLUIDS; ISSN 0045-7930; USA; DA. 1981; VOL. 9; NO 2; PP. 143-162; BIBL. 23 REF.Article

INTERACTION NON STATIONNAIRE DE L'ONDE DE CHOC AVEC UN CORPS EMOUSSE DANS UN COURANT SUPERSONIQUELYAKHOV VN.1979; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1979; NO 6; PP. 70-76; BIBL. 22 REF.Article

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