ON A MODEL FOR REENTRY ROLL RESONANCE. = MODELE DE LA RESONANCE EN ROULIS LORS D'UNE RENTREE ATMOSPHERIQUEKEVORKIAN J.1974; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1974; VOL. 26; NO 3; PP. 638-669; BIBL. 10 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

STUDY OF BASE PRESSURE IN LAMINAR HYPERSONIC FLOW: REENTRY FLIGHT MEASUREMENTS.BULMER BM.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 537; PP. 1-10; BIBL. 43 REF.Conference Paper

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

ANALYSIS OF R/V BEHAVIOR DURING BOUNDARY LAYER TRANSITION.CHRUSCIEL GT.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 109; PP. 1-25; BIBL. 23 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

EXTENSION OF THE MOMENTUM INTEGRAL METHOD TO THREE-DIMENSIONAL VISCOUS-INVISCID INTERACTIONS.GEORGEFF MP.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1603-1605; BIBL. 6 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

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

AERODYNAMIC HEATING ON 3-D BODIES INCLUDING THE EFFECTS OF ENTROPY-LAYER SWALLOURING.DEJARNETTE FR; HAMILTON HH.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 5-12; BIBL. 18 REF.Article

NATURE DE L'INFLUENCE DU NOMBRE DE REYNOLDS UNITAIRE SUR LA TRANSITION DANS UNE COUCHE LIMITE HYPERSONIQUEKHARITONOV AM; CHERNYKH VV.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 150-153; BIBL. 11 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

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

HYPERSONIC VISCOUS FLOW OVER A SLENDER CONE. II. TURBULENCE STRUCTURE OF THE BOUNDARY LAYER.LADERMAN AJ.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 534; PP. 1-11; BIBL. 18 REF.Conference Paper

INTEGRAL TECHNIQUE SOLUTIONS TO A CLASS OF SIMPLE ABLATION PROBLEMS.VALLERANI E.1974; MECCANICA; ITAL.; DA. 1974; VOL. 9; NO 2; PP. 94-101; ABS. ITAL.; BIBL. 5 REF.Article

HYPERSONIC VISCOUS FLOW OVER A SLENDER CONE. I. MEAN FLOW MEASUREMENTS.MARTELLUCCI A; LAGANELLI AL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 533; PP. 1-10; BIBL. 1 P.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

DERIVATION OF SHAPE CHANGE EQUATIONS FOR ASYMMETRICALLY HEATED ABLATING REENTRY VEHICLESNEURINGER JL.1973; INTERNATION. J. ENGNG SCI.; G.B.; DA. 1973; VOL. 11; NO 4; PP. 451-457; ABS. FR. ALLEM. RUSSE; BIBL. 2 REF.Serial Issue

EXPERIMENTAL STUDY OF A HIGH LIFT RE-ENTRY VEHICLE CONFIGURATIONHOUWINK R; RICHARDS BE.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 749-751; BIBL. 5 REF.Serial Issue

NEWTONIAN AERODYNAMIC FORCES FROM POISSON'S EQUATIONPIKE J.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 499-504; BIBL. 12 REF.Serial Issue

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

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

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

BASIC FLUID DYNAMICSSHEN SF.1966; IN: SPACE MATH. PROC. SUMMER SEMIN. ITHACA, N.Y., 1963; PROVIDENCE, R.I.; AM. MATH. SOC.; DA. 1966; VOL. 3; PP. 1-53; BIBL. 7 REF.Conference Proceedings