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AILE TRIANGULAIRE DANS UN ECOULEMENT HYPERSONIQUEGOLUBINSKIJ AI; GOLUBKIN VN.1976; DOKL. AKAD. NAUK S.S.S.R.; S.S.S.R.; DA. 1976; VOL. 226; NO 4; PP. 789-790; BIBL. 6 REF.Article

PROPULSION OPTIONS FOR THE HYPERSONIC RESEARCH AIRPLANE.VAN CAMP VV; WILLIAMS ET.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 611-616; BIBL. 16 REF.Article

OPTIMAL LIFT CONTROL BY MIELE'S METHOD FOR THE ATMOSPHERIC ENTRY OF A HYPERSONIC GLIDER. II. ISOPERIMETRIC TYPE PROBLEMSBEINER L.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 5; PP. 1039-1053; BIBL. 2 REF.Serial Issue

MINIMISATION DE LA RESISTANCE DE CORPS EN ETOILE DANS UN ECOULEMENT HYPERSONIQUE DE GAZKRAVETS VV; NYIKOLAJEV SV.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 1; PP. 40-43; ABS. ANGL. RUSSE; BIBL. 2 REF.Article

HIGHER ORDER SIMILARITY SOLUTIONS FOR HYPERSONIC AEROFOILS.HUI WH; HEMDAN HT.sdIN: SYMMETRY, SIMILARITY GROUP THEOR. METHODS MECH. PROC. SYMP.; CALGARY; 1974; S.L.; DA. S.D.; PP. 403-417; BIBL. 7 REF.Conference Paper

LOI DES SECTIONS TRANSVERSALES POUR UNE COUCHE LIMITE TRIDIMENSIONNELLE SUR UNE AILE MINCE DANS UN ECOULEMENT HYPERSONIQUEDUDIN GN; NEJLAND V YA.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 2; PP. 75-84; BIBL. 6 REF.Article

CALCUL DE L'ECOULEMENT HYPERSONIQUE AUTOUR D'UN CORPS A CASSURE DE LA GENERATRICE EN TENANT COMPTE DU TRANSPORT BIDIMENSIONNEL DU RAYONNEMENTZNAMENSKIJ VV.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 2; PP. 114-121; BIBL. 9 REF.Article

EINIGE UNTERSUCHUNGEN AN FLUGKOERPERN MIT ZENTRALSTIFT ALS STEUERORGAN BEI HOHEN MACHZAHLEN. = QUELQUES ETUDES DE MISSILES AYANT UNE POINTE COMME ORGANE DE COMMANDE AUX MEMBRES DE MACH ELEVESWYBORNY W.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 3; PP. 1-30; ABS. ANGL.; BIBL. 7 REF.Serial Issue

CALCULATED HEATING ON THE AFTERBODY NOZZLE OF A HYPERSONIC AIRCRAFT CONCEPT.TALCOTT NA JR; HUNT JL.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 12; PP. 1247-1248; BIBL. 7 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

HEATING AUGMENTATION IN EROSIVE HYPERSONIC ENVIRONMENTS.DUNBAR LE; COURTNEY JF; MCMILLEN LD et al.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 908-912; BIBL. 10 REF.Article

HOLOGRAPHIC ANALYSIS OF PARTICLE-INDUCED HYPERSONIC BOW-SHOCK DISTORSIONS.HOVE DT; SMITH AA.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 947-949; BIBL. 5 REF.Article

A CORRELATION BETWEEN PRESSURE AND HEAT TRANSFER DISTRIBUTIONS AT SUPERSONIC AND HYPERSONIC SPEEDS.STOLLERY JL; COLEMAN GT.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 4; PP. 304-312Article

CROSS-HATCHING STUDIES. A CRITICAL REVIEW.SWIGART RJ.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1301-1318; BIBL. 46 REF.Article

INTEGRAL APPROXIMATION FOR SLENDER-BODY SHOCK SHAPES IN HYPERSONIC FLOW.FIORINO TD; RASMUSSEN ML.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1735-1737; BIBL. 8 REF.Article

ETUDE THEORIQUE ET EXPERIMENTALE DE LA GEOMETRIE D'INJECTIONS SONIQUES DANS UN ECOULEMENT HYPERSONIQUE.BELLAIR MA.1974; ; S.L.; DA. 1974; PP. 1-42; H.T. 22; BIBL. 2 P.; (THESE DOCT. 3E CYCLE, SPEC. PHYS., MENTION MEC. FLUIDES; PARIS VI)Thesis

INSTABILITE DE L'ECOULEMENT HYPERSONIQUE AUTOUR D'UN COIN DANS L'APPROCHE NEWTONIENNEAPSHTEJN EH Z; GILINSKIJ MM.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 4; PP. 158-160; BIBL. 5 REF.Article

INSTALLATION GAZO-DYNAMIQUE FONCTIONNANT EN IMPULSIONS DU TYPE CIRCULAIRESKIBENKO EI; YUFEROV VB.1976; PRIBORY TEKH. EKSPER.; S.S.S.R.; DA. 1976; NO 4; PP. 237-238Article

SHOCK EXPANSION ANALYSIS OF HYPERSONIC PISTONS DECELERATING IN LONG TUBES. = ANALYSE DU DEVELOPPEMENT D'ONDES DE CHOC PAR DES PISTONS HYPERSONIQUES DECELERANT DANS DE LONGS TUBESHICKMAN RS.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1404-1406; BIBL. 6 REF.Article

SOLUTION OF MAXWELL'S MOMENT EQUATIONS BY THE METHOD OF RATIONAL TRUNCATION AND COORDINATE STRAINING.BAGANOFF D; ELLIOTT JP.1975; PHYS. OF FLUIDS; U.S.A.; DA. 1975; VOL. 18; NO 12; PP. 1660-1665; BIBL. 8 REF.Article

EXPERIMENTELLE UNTERSUCHUNGEN DES WAERMEUEBERGANGES AN STUMPFEN KEGELN IN HYPERSONISCHEN STROEMUNGEN BEI SEHR GERINGEN DICHTEN. = ETUDES EXPERIMENTALES DU TRANSFERT DE CHALEUR SUR DES CONES TRONQUES PLACES DANS UN ECOULEMENT HYPERSONIQUE, A TRES BASSE DENSITEBACHOUR F; ERDTEL D.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 28; PP. 1-53; ABS. ANGL.; BIBL. 3 P.Article

SUR LA FORME D'UN CORPS DE RESISTANCE MINIMALE DANS UN ECOULEMENT HYPERSONIQUEBERDICHEVSKIJ VL.1975; VEST MOSKOV. UNIV., 1; S.S.S.R.; DA. 1975; VOL. 30; NO 3; PP. 90-96; ABS. ANGL.; BIBL. 4 REF.Article

AERODYNAMIC HEATING ON 3-D BODIES INCLUDING THE EFFECTS OF ENTROPY-LAYER SWALLOWING.DEJARNETTE FR; HAMILTON HH.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 602; PP. 1-9; H.T. 3; BIBL. 16 REF.Conference Paper

LARGE INCIDENCE HYPERSONIC SIMILITUDE AND OSCILLATING NONPLANAR WEDGESKUNAL GHOSH; BINOY KRISHNA MISTRY.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 1004-1006; BIBL. 11 REF.Article

THE FLOW OF AN INFINITE COMPRESSIBLE FLUID PAST A RIGID, GRAVITATING SPHERE AND INTERACTING DEGENERATE STAR-RED GIANT BINARIESSHARA MM; SHAVIV G.1980; ASTROPHYS. SPACE SCI.; NLD; DA. 1980; VOL. 67; NO 2; PP. 427-443; BIBL. 19 REF.Article

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