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

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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

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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

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

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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

ANALYSIS OF HIGH-VELOCITY AND REAL-GAS EFFECTS ON THE SHOCK-INTERFERENCE PATTERN FOR DELTA-WING ORBITERS.BERTIN JJ; GRAUMANN BW; GOODRICH WD et 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. 522; PP. 1-10; BIBL. 12 REF.Conference Paper

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

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

FLOWFIELD MEASUREMENTS IN AN ASYMMETRIC AXIAL CORNER AT M=12.5.COOPER JR; HANKEY WL JR.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1353-1357; BIBL. 7 REF.Article

STAGNATION AND DOWNSTREAM VISCOUS SHOCKLAYER SOLUTIONS WITH RADIATION AND COUPLED ABLATION INJECTION.MOSS JN.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 73; PP. 1-11; BIBL. 16 REF.Conference Paper

EXPERIMENTELLE ERGEBNISSE ZUM NONWEILER-WELLENREITER IM UNTERSCHALL-, TRANSSCHALL- UND UBERSCHALLBEREICH = RESULTATS D'ETUDE EXPERIMENTALE SUR UNE AILE "NONWEILER" DANS LES DOMAINES SUBSONIQUE, TRANSSONIQUE ET SUPERSONIQUEGANZER U.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 5; PP. 153-159; ABS. ANGL. FR.; BIBL. 11 REF.Serial Issue

HYDRODYNAMIC STABILITY OF RE-ENTRY FLOWSWANG SY; FOX JA.1972; IN: DEV. THEOR. APPL. MECH. PROC. 6TH SOUTHEAST. CONF. TAMPA, FLA, 1972; TAMPA, FLA; 6TH SOUTHEAST. CONF. THEOR. APPL. MECH.; DA. 1972; VOL. 6; PP. 311-328; BIBL. 19 REF.Conference Proceedings

HYPERSONIC, TURBULENT SKIN-FRICTION AND HEAT-TRANSFER MEASUREMENTS ON A SHARP CONE.KUEI YUAN CHIEN.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1522-1526; BIBL. 27 REF.Article

CARACTERISTIQUES AERODYNAMIQUES DES CORPS DE REVOLUTION DANS LES CONDITIONS D'ECOULEMENT SUIVANT LA "LOI DE LOCALITE"BUNIMOVICH AI.1974; VEST. MOSKOV. UNIV., 1; S.S.S.R.; DA. 1974; VOL. 29; NO 4; PP. 97-102; ABS. ANGL.; BIBL. 5 REF.Article

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