HYPERSONIC VISCOUS FLOW OVER A SLENDER CONE. III. LAMINAR INSTABILITY AND TRANSITION.DEMETRIADES A.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 535; PP. 1-9; BIBL. 10 REF.Conference Paper

COMPARISON OF TRANSITION AND FREESTREAM DISTURBANCE MEASUREMENTS OBTAINED IN TWO WIND TUNNEL FACILITIES.OWEN FK; HORSTMAN CC; STAINBACK PC et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 131; PP. 1-4; BIBL. 7 REF.Conference Paper

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

MIXING LAYERS FOR HIGHLY UNDEREXPANDED SUPERSONIC JETS IN HYPERSONIC STREAMS.MORAN JP.1974; J. FLUID MECH.; G.B.; DA. 1974; VOL. 65; NO 1; PP. 153-175; BIBL. 1 P. 1/2Article

AN EXPERIMENTAL STUDY OF HYPERSONIC WAKES BEHIND WEDGES AT ANGLE OF ATTACKJIUNN JENQ WU; BEHRENS W.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1582-1589; BIBL. 23 REF.Serial Issue

INFLUENCE OF MODERATE WALL COOLING ON CONE TRANSITION AT M_E=13.7 IN HELIUMFISCHER MC.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 282-283; BIBL. 14 REF.Serial Issue

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

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

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

ECOULEMENT HYPERSONIQUE AUTOUR DE CORPS POINTUS ET EMOUSSES AVEC UNE GENERATRICE CONCAVEVISHNEVETSKIJ SL; PAKHOMOVA ZS.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 1; PP. 176-180; BIBL. 5 REF.Article

A NON-UNIQUENESS OF THE HYPERSONIC BOUNDARY LAYER.BROWN SN; STEWARTSON K.1975; QUART. J. MECH. APPL. MATH.; G.B.; DA. 1975; VOL. 28; NO 1; PP. 75-90; BIBL. 19 REF.Article

ETUDE DES PROJECTILES EN VOL HYPERSONIQUE ET DE LEURS SILLAGES PAR DES METHODES HOLOGRAPHIQUES.SMIGIELSKI P.1973; AO-CNRS-10877; FR.; DA. 1973; PP. (245P.); BIBL. 6 P.; (THESE DOCT. SCI. PHYS.; BESANCON)Thesis

REMOTE SENSING OF CF₄ NUMBER DENSITY IN A HYPERSONIC FLOW USING RAMAN SCATTERING = MESURE A DISTANCE DE LA DENSITE EN NOMBRE DE CF₄ RESIDUEL DANS UN ECOULEMENT HYPERSONIQUE UTILISANT LA TECHNIQUE DE DIFFUSION RAMANHILLARD ME JR; EMORY ML; BANDY AR et al.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 6; PP. 775-776; BIBL. 3 REF.Serial Issue

ASYMMETRIC NOSE BLUNTNESS EFFECTS ON THE AERODYNAMICS OF A SLENDER CONE AT MACH 14 = EFFETS D'EMOUSSEMENT ASYMETRIQUE DE LA POINTE SUR L'AERODYNAMIQUE D'UN CONE ELANCE A MACH 14WALCHNER O.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-6; BIBL. 5 REF.Conference Paper

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

THE NUMERICAL SOLUTION OF CONVECTIVE HEAT TRANSFER IN THE SPACE SHUTTLE BASE REGION BY TELENIN'S METHODHENG JCS.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 191-200; BIBL. 7 REF.; (PROC. 3RD INT. CONF. NUMER. METHODS FLUID MECH II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

PERIODICITY IN EXOTHERMIC HYPERSONIC FLOWS ABOUT BLUNT PROJECTILESALPERT RL; TAU YI TOONG.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 4-5; PP. 539-560; ABS. FR. RUSSE; BIBL. 18 REF.Serial Issue

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

A CATALOGUE OF EUROPEAN HYPERSONIC WIND TUNNEL FACILITIES.1975; AGARD-R-619; FR.; DA. 1975; PP. (55P.)Report

WIND TUNNEL EXPERIMENTS RELATING TO SUPERSONIC AND HYPERSONIC BOUNDARY LAYER TRANSITION.KENDALL JM.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 133; PP. 1-13; BIBL. 23 REF.Conference Paper

PROBLEME DE LA TRAINEE D'UN SYSTEME DE DEUX SPHERES SE DEPLACANT A VITESSE HYPERSONIQUE DANS UN MILIEU MOLECULAIRE LIBRE, PERPENDICULAIRE A L'AXE RELIANT LEURS CENTRESKOSOWSKI S.1974; POST. ASTRONAUT., BIUL. NAUK.; POLSKA; DA. 1974; VOL. 7; NO 4; PP. 61-99; ABS. RUSSE ANGL.; BIBL. 7 REF.Article

SCHLIEREN VISUALIZATION OF THE HYPERSONIC ENTROPY WAKEGIESBRECHT H; STILP A; MERZKIRCH W et al.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1694-1695; BIBL. 5 REF.Serial Issue

BASE PRESSURE DISTRIBUTION OF A CONE AT HYPERSONIC SPEEDSPICK GS.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1685-1686; BIBL. 4 REF.Serial Issue

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