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CONCEPTUAL DESIGN OF A LIFT FAN PLUS LIFT/CRUISER FIGHTER AIRCRAFT.HILL GC; WATERS MH.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 10; PP. 763-768; BIBL. 8 REF.Article

DESIGN STUDY OF STRUCTURAL CONCEPTS FOR AN ARROW-WING SUPERSONIC-CRUISE AIRCRAFT.SAKATA IF; DAVIS GW; ROBINSON JC et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1037; PP. 1-12; BIBL. 3 REF.Conference Paper

TECHNIQUES FOR DETERMINING PROPULSION SYSTEM FORCES FOR ACCURATE HIGH SPEED VEHICLE DRAG MEASUREMENTS IN FLIGHT.ARNAIZ HH.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 964; PP. 1-13; BIBL. 6 REF.Conference Paper

PROPELLANTS SELECTION TO PROVIDE AN AIR SIMULANT FOR HOT GAS TESTING OF RAMJETSMITCHELL W.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1070; PP. 1-5; BIBL. 3 REF.Conference Paper

INTERACTION DE DEUX EMETTEURS ACOUSTIQUES SE DEPLACANT A UNE VITESSE SUPERSONIQUEGRIGOR'EV GI; DOKUCHAEV VP; EHJDMAN V YA et al.1976; AKUST. ZH.; S.S.S.R.; DA. 1976; VOL. 22; NO 1; PP. 127-129; BIBL. 6 REF.Article

EFFECT OF FOREBODY SHAPE AND SHIELDING TECHNIQUE ON 2-D SUPERSONIC INLET PERFORMANCE.SURBER LE.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1183; PP. 1-19; BIBL. 8 REF.Conference Paper

AEROELASTIC PANEL OPTIMIZATION WITH AERODYNAMIC DAMPING.PIERSON BL.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 515-517; BIBL. 12 REF.Article

SUR UN PROBLEME DE DIFFRACTION D'UNE ONDE DE CHOC SUR UN COIN MOBILE AVEC UN SAUT DE DENSITE ASSOCIEBEZHANOV KA.1974; IN: SIMP. MEKH. SPLOSHNOJ SREDY RODSTVENNYM PROBL. ANAL. TR.; TBILISI; 1971; TBILISI; METSNIEVERA; DA. 1974; VOL. 2; PP. 36-45; BIBL. 16 REF.Conference Paper

SUPERSOMIC NEUTRAL WINDS IN AN OUTER ATMOSPHERE. I. ISOTHERMAL CONDITIONS.GILBERT NE; COLE KD.1974; AUSTRAL. J. PHYS.; AUSTRAL.; DA. 1974; VOL. 27; NO 4; PP. 511-528; BIBL. 38 REF.Article

ON A HYPERSONIC LAUNCHING SYSTEM. = SYSTEME DE LANCEMENT HYPERSONIQUEWLODARCZYK E.1976; J. TECH. PHYS.; POLAND; DA. 1976; VOL. 17; NO 1; PP. 71-79; ABS. POL. RUSSE; BIBL. 7 REF.Article

UNSTEADY SUPERSONIC CASCADE IN SUBSONIC AXIAL FLOW.VERDON JM; MCCUNE JE.1975; A.I.A.A., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 2; PP. 193-201; BIBL. 19 REF.Article

APPLICATION OF AN ADVANCED COMPUTERIZED STRUCTURAL DESIGN SYSTEM TO AN ARROW-WING SUPERSONIC CRUISE AIRCRAFT.ROBINSON JC; YATES EC JR; TURNER MJ et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1038; PP. 1-9; H.T. 2; BIBL. 19 REF.Conference Paper

DESTRUCTION DU RECOUVREMENT DE PROTECTION THERMIQUE EN TEFLON POUR DES VITESSES SUPERSONIQUES DE VOLPROZOROVA EH V; REZNIKOV BI.1974; P.M.T.F.; S.S.S.R.; DA. 1974; NO 4; PP. 94-100; BIBL. 11 REF.Article

A SYSTEMATIC STUDY OF SUPERSONIC JET NOISE = ETUDE SYSTEMATIQUE DU BRUIT D'UN JET SUPERSONIQUELOUIS JF; LETTY RP; PATEL JR et al.1972; IN: AIAA 5TH FLUID PLASMA DYN. CONF. BOSTON, MASS., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 641; PP. 1-11; BIBL. 12 REF.Conference Paper

SIMPLIFIED ANALYSIS OF SUPERSONIC BASE FLOWS INCLUDING INJECTION AND COMBUSTION.SCHETZ JA; BILLIG FS; FAVIN S et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 1; PP. 7-8; BIBL. 6 REF.Article

STATISCHE STABILITAET UND APERIODISCHE INSTABILITAET IM UNTER-UND UEBERSCHALL. = STABILITE STATIQUE ET INSTABILITE APERIODIQUE EN SUBSONIQUE ET EN SUPERSONIQUESACHS G.1975; Z. FLUGWISSENSCH.; DTSCH.; DA. 1975; VOL. 23; NO 10; PP. 341-346; ABS. ANGL. FR.; BIBL. 12 REF.Article

VISUALISATION PAR HOLOGRAPHIE ULTRA-RAPIDE DU RELIEF D'UN SILLAGE DE PROJECTILE EN VOL A MACH 2.FAGOT H; SMIGIELSKI P; SIMON G et al.1974; ISL-CO-17-74; FR.; DA. 1974; ABS. ANGL.; BIBL. 3 REF.; (11E CONGR. INT. PHOTOGR. ULTRA-RAPIDE; LONDRES; 1974)Conference Proceedings

SUPERSONIC GENERATION OF ATMOSPHERIC WAVESBEER T.1973; NATURE; G.B.; DA. 1973; VOL. 242; NO 5392; PP. 34; BIBL. 7 REF.Serial Issue

STROEMUNGEN UM TRAGFLAECHEN IM STATIONAEREN UEBERSCHALLFLUG. IHRE DARSTELLUNG UND BERECHNUNG AUF DER GRUNDLAGE VON AUFTRIEBS-AUFWINDBEZIEHUNGEN. = ECOULEMENTS AUTOUR DE SURFACES PORTANTES EN ECOULEMENT STATIONNAIRE SUPERSONIQUE. REPRESENTATION ET CALCUL A PARTIR DES RELATIONS ENTRE FORCE ASCENSIONNELLE ET VENT ASCENDANTLEITER E.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 61; PP. 1-125; ABS. ANGL.; BIBL. 9 P. 1/2Serial Issue

SUPERSONIC NEUTRAL WINDS IN AN OUTER ATMOSPHERE. II. EFFECTS OF VARIABLE TEMPERATURE.GILBERT NE; COLE KD.1974; AUSTRAL. J. PHYS.; AUSTRAL.; DA. 1974; VOL. 27; NO 4; PP. 529-540; BIBL. 7 REF.Article

MOUVEMENT TRIDIMENSIONNEL NON STATIONNAIRE D'UN APPAREIL VOLANT RENTRANT DANS L'ATMOSPHERE A VITESSE SUPERSONIQUEGROBOV VA; KOTSYUBA AV.1972; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1972; VOL. 8; NO 12; PP. 71-79; BIBL. 6 REF.Serial Issue

THE FLOW OVER A "HIGH" ASPECT RATIO GOTHIC WING AT SUPERSONIC SPEEDS.YEGNA NARAYAN K.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 3; PP. 189-201; BIBL. 10 REF.Article

MOVING LOAD ON A LAMINATED COMPOSITE.SVE C; HERRMANN G.1974; J. APPL. MECH.; U.S.A.; DA. 1974; VOL. 41; NO 3; PP. 663-667; BIBL. 11 REF.Article

DIFFRACTION D'UNE ONDE PLANE SUR UN COIN SE DEPLACANT A VITESSE SUPERSONIQUE, DANS LE CAS D'UNE INTERACTION AVEC UNE ONDE DE CHOC IRREGULIEREPEKUROVSKIJ LE; TER MINASYANTS SM.1974; PRIKL. MAT. MEKH.; S.S.S.R.; DA. 1974; VOL. 38; NO 3; PP. 484-493; BIBL. 14 REF.Article

ANALYSE GENERALE DE LA CARTE DE LA DIFFRACTION D'UNE ONDE ACOUSTIQUE PLANE SUR UN COIN SE DEPLACANT A UNE VITESSE SUPERSONIQUEPANASENKO AV.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 172-175; BIBL. 5 REF.Article

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