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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

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

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

REGIMES AUTOSIMILAIRES DES COLLAPSUS D'ONDESZAKHAROV VE; SHCHUR LN.1981; Z. EKSP. TEOR. FIZ.; ISSN 0044-4510; SUN; DA. 1981; VOL. 81; NO 6; PP. 2019-2031; ABS. ENG; BIBL. 22 REF.Article

ETUDE DE LA COLLISION D'UN LIEN FLEXIBLE ET D'UN CORPS EMOUSSEAGALAROV DG; MUTALLIMOV SH M.1972; IZVEST. AKAD. NAUK AZERBAJDZH. S.S.R., FIZ.-TEKH. MAT. NAUK; S.S.S.R.; DA. 1972; NO 4; PP. 43-45; ABS. AZERB. ANGL.; BIBL. 3 REF.Serial Issue

ALTITUDE TRANSITIONS IN ENERGY CLIMBWESTON AR; CLIFF EM; KELLEY HJ et al.1983; AUTOMATICA (OXFORD); ISSN 0005-1098; GBR; DA. 1983; VOL. 19; NO 2; PP. 199-202; BIBL. 16 REF.Article

AN EFFECTIVE ENVIRONMENTAL CONTROL SYSTEM FOR A SUPERSONIC AIR LAUNCHED MISSILEGONZALEZ JI.1980; INSTRUMENTATION IN THE AEROSPACE INDUSTRY. ADVANCES IN TEST MEASUREMENT. INTERNATIONAL INSTRUMENTATION SYMPOSIUM. 26/1980/SEATTLE WA; USA; RESEARCH TRIANGLE PARK NC: INSTRUMENT SOCIETY OF AMERICA; DA. 1980; VOL. 2; PP. 543-552; BIBL. 1 REF.Conference Paper

HIGH-VELOCITY FEATURES IN M42 DRIVEN BY STELLAR WINDSTAYLOR K; MUNCH G.1978; ASTR. AND ASTROPHYS.; DEU; DA. 1978; VOL. 70; NO 3; PP. 359-366; BIBL. 34 REF.Article

ROLE DE LA COMPRESSIBILITE DANS LE PROCESSUS D'INTERACTION A GRANDE VITESSE ENTRE CORPS SOLIDESZLATIN NA; KOZHUSHKO AA.1980; FIZ. GOREN. VZRYVA; ISSN 0430-6228; SUN; DA. 1980; VOL. 16; NO 5; PP. 94-96; BIBL. 13 REF.Article

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