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Results 1 to 25 of 1362

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OPTIMAL AERODYNAMIC CONTROL BY MATCHED ASYMPTOTIC EXPANSIONS.FROSTIC F; VINH NX.1976; ACTA ASTRONAUT.; G.B.; DA. 1976; VOL. 3; NO 5-6; PP. 319-332; BIBL. 4 REF.Article

TURBULENT BOUNDARY-LAYER FLOW OVER RE-ENTRY BODIES INCLUDING ROUGHNESS EFFECTSGOGINENI PR.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1758-1760; BIBL. 12 REF.Article

OPTIMUM RE-ENTRY CONFIGURATION VIA THE METHOD OF STEEPEST DESCENTTAWAKLEY VB.1978; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROM; DA. 1978; VOL. 23; NO 4; PP. 521-530; BIBL. 6 REF.Article

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

ANGLE-OF-ATTACK CONTROL OF DRAG FOR SLENDER RE-ENTRY VIHICLE RECOVERY.PLATUS DH.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 275-281; BIBL. 9 REF.Article

A METHOD FOR THE STUDY OF NON-OSCILLATORY CIRCULAR LIFTING RE-ENTRIESBEINER L.1978; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROM; DA. 1978; VOL. 23; NO 4; PP. 531-544; BIBL. 3 REF.Article

ON THE STATE AND PARAMETER ESTIMATION FOR MANEUVERING REENTRY VEHICLES.CHAW BING CHANG; WHITHING RH; ATHANS M et al.1977; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1977; VOL. 22; NO 1; PP. 99-105; BIBL. 21 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

INVISCID FLOWFIELD CALCULATIONS FOR RE-ENTRY VEHICLES WITH CONTROL SURFACES.SOLOMON JM; CIMENT M; FERGUSON RE et al.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 1742-1749; BIBL. 20 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

MEMBRANE FACTORS IN ARRHYTHMOGENESIS. CONCEPTS AND DEFINITIONS.ARNSDORF MF.1977; PROGR. CARDIOVASCUL. DIS.; U.S.A.; DA. 1977; VOL. 19; NO 6; PP. 413-429; BIBL. 4 P.Article

NONINVASIVE DIAGNOSIS OF DUAL AV NODAL PATHWAYS WITH INABILITY TO PARTICIPATE IN REENTRANT TACHYCARDIABUMP TE; GALLASTEGUI J; BAUERNFEIND RA et al.1983; CHEST; ISSN 0012-3692; USA; DA. 1983; VOL. 83; NO 6; PP. 918-920; BIBL. 9 REF.Article

Purkinje-Related Arrhythmias Part I: Monomorphic Ventricular TachycardiasNOGAMI, Akihiko.Pacing and clinical electrophysiology. 2011, Vol 34, Num 5, pp 624-650, issn 0147-8389, 27 p.Article

SHOCK STRENGTH MODIFICATION FOR REDUCED HEAT TRANSFER TO LIFTING RE-ENTRY VEHICLESTOWNEND LH; EAST RA.1982; SHOCK TUBES AND WAVES. INTERNATIONAL SYMPOSIUM ON SHOCK TUBES AND WAVES. 13 /1981-07-06/NIAGARA FALLS NY; USA; ALBANY: STATE UNIVERSITY OF NEW YORK PRESS; DA. 1982; PP. 367-375; BIBL. 18 REF.Conference Paper

OBSERVATIONS ON SPONTANEOUS TERMINATION OF ATRIOVENTRICULAR NODAL REENTRANT TACHYCARDIABRUGADA P; ROSS D; BAR FWHM et al.1981; AM. J. CARDIOL.; ISSN 0002-9149; USA; DA. 1981; VOL. 47; NO 3; PP. 703-707; BIBL. 12 REF.Article

THE HYPERSONIC FLOW FIELD OVER A RUNTRY VEHICLE INDENTED NOSE CONFIGURATIONMORRISON AM; YANTA WJ; VOISINET RLP et al.1981; THERMOPHYSICS CONFERENCE. 16/1981-06-23/PALO ALTO CA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 12 P.; BIBL. 15 REF.Conference Paper

INTRAVENTRICULAR REENTRY WITH NARROW QRS COMPLEXREDDY CP; KHORASANCHIAN A.1980; CIRCULATION; USA; DA. 1980; VOL. 61; NO 3; PP. 641-647; BIBL. 29 REF.Article

VENTRICULAR TACHYCARDIA IN INFANCY: EVIDENCE FOR A REENTRANT MECHANISMGAUM WE; SCHWARTZ DC; KAPLAN S et al.1980; CIRCULATION; ISSN 0009-7322; USA; DA. 1980; VOL. 62; NO 2; PP. 401-406; BIBL. 16 REF.Article

THE FAST-SLOW FORM OF ATRIOVENTRICULAR NODAL REENTRANT TACHYCARDIA IN CHILDRENWOLFF GS; SUNG RJ; PICKOFF A et al.1979; AMER. J. CARDIOL.; USA; DA. 1979; VOL. 43; NO 6; PP. 1181-1188; BIBL. 35 REF.Article

LOW TEMPERATURE SIMULATION OF SUBLIMING BOUNDARY-LAYER FLOW IN JUPITER ATMOSPHERE.CHING JEN CHEN.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 3; PP. 259-267; BIBL. 24 REF.Article

HEAT-TRANSFER MEASUREMENTS IN SEPARATED LAMINAR BASE FLOW.BULMER BM.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 11; PP. 701-702; BIBL. 13 REF.Article

MECHANISMS OF ATRIOVENTRICULAR JUNCTIONAL TACHYCARDIA. ROLE OF REENTRY AND CONCEALED ACCESSORY BYPASS TRACTS.BAROLD SS; COUMEL P.1977; AMER. J. CARDIOL.; U.S.A.; DA. 1977; VOL. 39; NO 1; PP. 97-106; BIBL. 2 P. 1/2Article

EFFECTS OF ATOMIC OXYGEN ON GRAPHITE ABLATION.CHUL PARK.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 11; PP. 1640-1642; BIBL. 23 REF.Article

FLIGHT-TEST BASE PRESSURE MEASUREMENTS IN TURBULENT FLOW.BULMER BM.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 12; PP. 1783-1785; BIBL. 9 REF.Article

MULTISENSOR TRACKING OF RE-ENTRY VEHICLES.SMITH FW; SPAIN DS.1976; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 15. PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 575-578; BIBL. 2 REF.Conference Paper

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