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THE EFFECTS OF RECESSED LOWER SURFACE SHAPE ON THE LIFT AND DRAG OF CONICAL WINGS AT HIGH INCIDENCE AND HIGH MACH NUMBER.SQUIRE LC.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 1; PP. 1-10; BIBL. 6 REF.Article

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

THE EFFECT OF SURFACE ROUGHNESS CHARACTER ON TURBULENT RE-ENTRY HEATINGFINSON ML; CLARKE AS.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; PP. 83-108; BIBL. 17 REF.Conference Paper

FREIFLUGVERSUCHE MIT FERNGESTEUERTEN MODELLEN VON WIEDEREINTRITTSKOERPERN. = ESSAIS EN VOL SUR DES MODELES TELEGUIDES DE CORPS RENTRANT DANS L'ATMOSPHERERUNNE K.1975; RAUMFAHRTFORSCHUNG; DTSCH.; DA. 1975; VOL. 19; NO 6; PP. 308-313; ABS. ANGL.; BIBL. 13 REF.Article

THEORY OF LANGMUIR PROBE USED IN A RE-ENTRY VEHICLE SURROUNDED BY A FLOWING CONTINUUM PLASMA.VASISHTH SHARMA; VERMA JS.1973; J. INSTIT. ELECTRON. TELECOMMUNIC. ENGRS; INDIA; DA. 1973; VOL. 19; NO 7; PP. 378-386; BIBL. 11 REF.Article

EXPERIMENTAL INVESTIGATION OF SUPERSONIC FLOW PAST DOUBLE-WEDGE CONFIGURATIONS.BERTIN JJ; HINKLE JC.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 897-901; BIBL. 8 REF.Article

STUDY OF BASE PRESSURE IN LAMINAR HYPERSONIC FLOW: RE-ENTRY FLIGHT MEASUREMENTS. = ETUDE DE LA PRESSION DE CULOT EN ECOULEMENT LAMINAIRE HYPERSONIQUE: MESURES EN VOL DE RENTREEBULMER BM.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1340-1348; BIBL. 1 P.Article

AERODYNAMISCHE WIEDEREINTRITTSPROBLEME IN WINDKANALANLAGEN BEI SEHR GERINGER DICHTE UND GROSSER ENERGIE. = PROBLEMES AERODYNAMIQUES DE RENTREE DANS L'ATMOSPHERE TRAITES EN SOUFFLERIE, A TRES BASSE DENSITE ET A HAUTE ENERGIEBECKER M.1975; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1975; VOL. 75; NO 16; PP. 1-59; ABS. ANGL.; BIBL. 2 P.Serial Issue

SIMULATION OF HIGH ALTITUDE FLIGHT IN WIND-TUNNELS AND CORRELATION OF FREE-FLIGHT AND WIND TUNNEL DATA.WUEST W.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 357-368; BIBL. 1 P. 1/2Conference Paper

MOUVEMENT DANS L'ATMOSPHERE DE CORPS GAZEUX DE FAIBLE DENSITEKUTSAEV AS.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1978; NO 2; PP. 89-93; BIBL. 6 REF.Article

EFFECTS OF POROUS RINGS ON THE AERODYNAMIC CHARACTERISTICS OF A SPHERE.CAHEN GL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 572-574Article

UN MOYEN DE GUIDAGE DES APPAREILS EN VOL HYPERSONIQUEZHURAVSKIJ VR; MAMATOV VP; SKORIK AD et al.1976; KOSM. ISSLEDOV. UKRAINE; S.S.S.R.; DA. 1976; NO 8; PP. 43-48; BIBL. 9 REF.Article

AEROTHERMODYNAMICS AND PLANETARY ENTRY. TECHNICAL PAPERS FROM THE AIAA 18TH AEROSPACE SCIENCES MEETING, JANUARY 1980CROSBIE AL ED.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; 461 P.; BIBL. DISSEM.Conference Paper

IONIZATIONAL NONEQUILIBRIUM HEATING DURING OUTER PLANETARY ENTRIES.LEIBOWITZ LP; TA JIN KUO.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 9; PP. 1324-1329; BIBL. 25 REF.Article

COMPUTATION OF THREE-DIMENSIONAL, INVISCID SUPERSONIC FLOWS.KUTLER P.1975; LECTURE NOTES PHYS.; GERM.; DA. 1975; NO 41; PP. 287-374; BIBL. 4 P.; (PROGR. NUMER. FLUID DYN. LECT. SER.; RHODE-ST.-GENESE, BELG.; 1974)Conference Paper

AMELIORATIONS DE LA SOUFFLERIE ARC II B DE L'O.N.E.R.A. POUR L'ETUDE DES PLASMAS DE RENTREE.FRITZ J.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 4; PP. 201-211; ABS. ANGL.; BIBL. 6 REF.Article

EFFETS DE FLECHE ET D'INCIDENCE SUR UNE AILE DELTA EN ECOULEMENT HYPERSONIQUE RAREFIE.DUROX D; ALLEGRE J.1975; AERONAUT. ET ASTRONAUT.; FR.; DA. 1975; NO 55; PP. 29-34; ABS. ANGL. ALLEM.; BIBL. 5 REF.Article

A PREDICTIVE MACROSCOPIC INTEGRAL RADIATION EFFICIENCY MODELREVELLE DO.1980; J. GEOPHYS. RES.; USA; DA. 1980; VOL. 85; NO B4; PP. 1803-1808; BIBL. 21 REF.Article

DECAY OF A HIGHLY ECCENTRIC SATELLITE.JANIN G; ROTH EA.1976; CELEST. MECH.; NETHERL.; DA. 1976; VOL. 14; NO 1; PP. 141-149; BIBL. 3 REF.; (CONF. MATH. METHODS CELESTIAL MECH. 5. PROC.; OBERWOLFACH; 1975)Conference Paper

RE-ENTRY VEHICLE BASE PRESSURE AND HEAT-TRANSFER MEASUREMENTS AT MINFINI=18.BULMER BM.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 522-524; BIBL. 9 REF.Article

DESIGN AND TESTING OF A CHEMICAL INJECTION SYSTEM FOR REENTRY PLASMA ALLEVIATION.LENNON JF; HERSKOVITZ SB.1974; AIR FORCE CAMBRIDGE RES. LAB., PHYS. SCI. RES. PAPERS; U.S.A.; DA. 1974; NO 588; PP. 1-48; BIBL. 1 P. 1/2Article

THERMAL STRESS ANALYSIS OF REENTRY VEHICLE NOSETIPS AT ANGLE OF ATTACKCROSE JG; MCKINLEY TK.1972; COMPUTERS AND STRUCT.; G.B.; DA. 1972; VOL. 2; NO 5-6; PP. 1031-1042; BIBL. 9 REF.Serial Issue

CARACTERISTIQUES AERODYNAMIQUES D'UN ELEMENT DE SURFACE SOUMISE A UN ECOULEMENT MOLECULAIRE A GRANDE VITESSEVARAKIN GK; FARAFONOV VG.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 4; PP. 181-184; BIBL. 8 REF.Article

A COMPARATIVE STUDY OF TIME-MARCHING AND SPACE-MARCHING NUMERICAL METHODSGUPTA RN; MOSS JN; SIMMONDS AL et al.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 145-147; BIBL. 15 REF.Article

FLOWFIELD CALCULATIONS PAST AN ENTRY PROBE WITH ABLATED NOSE SHAPEAJAY KUMAR; GRAVES RA JR; WEILMUENSTER KJ et al.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 6; PP. 719-720; BIBL. 4 REF.Article

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