EXPERIMENTAL STUDY OF SEPARATION FROM THE BASE OF A CONE AT SUPERSONIC SPEEDS.KAYSER LD; DANBERG JE.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1607-1609; BIBL. 8 REF.Article

ETUDE EXPERIMENTALE DES AILES NON PLANES AUX VITESSES SUPERSONIQUESBRODETSKIJ MD; KOSHCHEEV AB; CHEREMUKHIN GA et al.1974; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1974; NO 3; PP. 33-39; BIBL. 3 REF.Article

EINE GRAPHISH-ANALYTISCHE METHODE ZUR BESTIMMUNG DER OPTIMUM-OPTIMORUM-FORM DES DUENNEN DELTAFLUEGELS IN UEBERSCHALLSTROEMUNG. = METHODE GRAPHO-ANALYTIQUE POUR DETERMINER LA FORME OPTIMALE DE L'AILE DELTA MINCE EN ECOULEMENT SUPERSONIQUENASTASE A.1974; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1974; VOL. 19; NO 1; PP. 15-35; BIBL. 7 REF.Article

PROBLEMES D'INTERACTIONS ENTRE LA PRISE D'AIR ET L'AVION.LEYNAERT J.1974; CHATILLON; OFF. NATL. ETUD. RECH. AEROSP.; DA. 1974; PP. 1-11; ABS. ANGL.; BIBL. 25 REF.; (REUN. AGARD INTERFERENCE ENTRE CELL. PROPUL.; ROME; 1974)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

THREE DIMENSIONAL SUPERSONIC FLOW FIELD ANALYSIS OF THE B-1 AIRPLANE BY A FINITE DIFFERENCE TECHNIQUE AND COMPARISON WITH EXPERIMENTAL DATA.D'ATTORE L; BILYK MA; SERGEANT RJ et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 189; PP. 1-22; BIBL. 10 REF.Conference Paper

BOUNDARY LAYER TRANSITION ON SUPERSONIC CONES IN AN AEROBALLISTIC RANGE.POTTER JL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 132; PP. 1-13; BIBL. 21 REF.Conference Paper

PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 17-21; BIBL. 13 REF.Article

FINITE ELEMENT SUPERSONIC AERODYNAMICS FOR OSCILLATING PARALLEL WINGS.APPA K; SMITH GCC.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 433-434; BIBL. 11 REF.Article

OPTICAL EFFECTS OF SHOCK FRONT ON NOSE-MOUNTED OPTICS.STAUFFER DR.1974; APPL. OPT.; U.S.A.; DA. 1974; VOL. 13; NO 3; PP. 602-604; BIBL. 3 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES DES AILES DE GEOMETRIE COMPLEXE EN ECOULEMENT SUPERSONIQUEBOKOVIKOV YU G.1974; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1974; NO 8; PP. 48-55; BIBL. 10 REF.Article

PREDICTION OF TURBULENT HEAT TRANSFER AND PRESSURE ON SWEPT LEADING EDGES.COLEMAN HW; LEMMON EC.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 6; PP. 376-381; BIBL. 12 REF.Article

SUPERSONIC FLIGHT IN A STRATIFIED SHEARED ATMOSPHERE.SIROVICH L; CHONG TH.1974; PHYS. OF FLUIDS; U.S.A.; DA. 1974; VOL. 17; NO 2; PP. 310-320; BIBL. 28 REF.Article

THEORETICAL PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 111; PP. 1-8; BIBL. 11 REF.Conference Paper

AERODYNAMIC FORCES AND MOMENTS ON A SLENDER WITH A JET PLUME FOR ANGLES OF ATTACK UP TO 180 DEGREES.FLEEMAN EL; NELSON RC.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 110; PP. 1-15; BIBL. 25 REF.Conference Paper

THE SUPERSONIC FLOW AROUND A SHARP-NOSE ELLIPTIC CONE AT THE ANGLE OF ATTACK.VETLUTSKII VN; GANIMEDOV VL.1974; ARCH. MECH.; POLAND; DA. 1974; VOL. 26; NO 4; PP. 647-652; ABS. POL. RUSSE; BIBL. 7 REF.Article

OSCILLATORY SUPERSONIC KERNEL FUNCTION METHOD FOR ISOLATED WINGS.CUNNINGHAM AM JR.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 10; PP. 609-615; BIBL. 15 REF.Article

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

DEFLEXION NON STATIONNAIRE DE L'ECOULEMENT SUPERSONIQUE EN ARRIERE D'UNE AILE TRIANGULAIRESOLOMONYAN R SH.1972; IZVEST. AKAD. NAUK ARM. S.S.R., MEKH.; S.S.S.R.; DA. 1972; VOL. 25; NO 5; PP. 45-64; ABS. ARM. ANGL.; BIBL. 6 REF.Serial Issue

EXPERIMENTAL INVESTIGATIONS OF SEPARATED FLOWS ON WING-BODY COMBINATIONS WITH VERY SLENDER WINGS AT MACH NUMBERS M_INFINI=0.5 TO 2.2STAHL W; HARTMANN K; SCHNEIDER W et al.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 25; PP. 1-8; BIBL. 7 REF.Conference Paper

ON THE SHOCK-ON-SHOCK INTERACTION PROBLEM.KUTLER P; SAKELL L; AIELLO C 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. 524; PP. 1-11; BIBL. 24 REF.Conference Paper

TWO-DIMENSIONAL BOAT-TAILED BASES IN SUPERSONIC FLOW.VISWANATH PR; NARASIMHA R.1974; AERONAUT. QUART.; G.B.; DA. 1974; VOL. 25; NO 3; PP. 210-224; BIBL. 1 P.Article

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

CHARGES NON STATIONNAIRES REPARTIES SUR UNE AILE DE FORME EN PLAN ARBITRAIRE, DANS LE CAS D'UN MOUVEMENT SUPERSONIQUEMEZHLUMYAN RA; SOLOMONYAN R SH.1972; IZVEST. AKAD. NAUK ARM. S.S.R., MEKH.; S.S.S.R.; DA. 1972; VOL. 25; NO 3; PP. 41-59; ABS. ARM. ANGL.; BIBL. 7 REF.Serial Issue