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A THEORETICAL AND EXPERIMENTAL STUDY OF A JET STRETCHER SYSTEMBAUER RC; MATKINS EH; BAREBO RL et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-16; BIBL. 3 REF.Conference Paper

PRECOMBUSTION SHOCK STRUCTURE IN SCRAMJET ENGINESWALTRUP PJ; BILLIG FS.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 1181; PP. 1-8; BIBL. 12 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

CARACTERISTIQUES DES STATOREACTEURS DANS L'ATMOSPHERE DE LA PLANETRE MARSGOLAJDO LA; KORSUNOV YU A; TISHIN AP et al.1974; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1974; VOL. 17; NO 3; PP. 37-41; BIBL. 5 REF.Article

DESIGN, TESTS, AND VERIFICATION OF A DIFFUSER SYSTEM FOR A MACH 4 SCRAMJET TEST FACILITYANDREWS EH JR; MACKLEY EA.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 10; PP. 641-642Article

PARALLEL HYDROGEN INJECTION INTO CONSTANT-AREA, HIGH-ENTHALPY, SUPERSONIC AIRFLOWSTALKER RJ; MORGAN RG.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1468-1469; BIBL. 5 REF.Article

EXPERIMENTS ON METHODS FOR IMPROVED FUEL IGNITION IN SCRAMJET COMBUSTION SYSTEMSSUTTROP F.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 15; PP. 1-5; BIBL. 5 REF.Conference Paper

AN AERODYNAMIC STUDY OF SCRAMJET FUEL INJECTORSPAVINELLI LA.1974; IN: FLUID MECH. COMBUST. JT. FLUIDS ENG. CSME CONF., MONTREAL; 1974; NEW YORK; AM. SOC. MECH. ENG.; DA. 1974; PP. 115-133; BIBL. 6 REF.Conference Paper

BREVET 2.348.372 (A1) (76 10692). - 12 AVRIL 1976. CHAMBRE DE COMBUSTION, EN PARTICULIER POUR DES STATOREACTEURS.sdPatent

EAST ACTING HYDROGEN VALVEMORGAN RG; STALKER RJ.1983; JOURNAL OF PHYSICS E: SCIENTIFIC INSTRUMENTS; ISSN 0022-3735; GBR; DA. 1983; VOL. 16; NO 3; PP. 205-207; BIBL. 5 REF.Article

BREVET DISPOSITIF DE COMMANDE ET DE REGLAGE DE STATOREACTEURS A TURBINE A GAZ POUR AVIONS1978; ; FRA; DA. 1978-12-08; FR/A1/2.386-686; DEP.78 09517/1978-03-31; PR. DE/P 27 15300.0/1977-04-05Patent

RAMJET ENGINE TESTING AND SIMULATION TECHNIQUESDUNSWORTH LC; REED GJ.1979; J. SPACER. ROCK.; USA; DA. 1979; VOL. 16; NO 6; PP. 382-388; BIBL. 5 REF.Article

PROPULSION CONCEPTS FOR HIGH SPEED AIRCRAFT.STULL FD; JONES RA; ZIMA WP et al.1975; S.A.E. TRANS.; U.S.A.; DA. 1975 PARU 1976; VOL. 84; NO 4; PP. 3073-3087; BIBL. 14 REF.Article

CRUISE FLIGHT DURATION OF A LOW MACH NUMBER RAMJETHATTINGH HV.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 6; PP. 425-430; BIBL. 10 REF.Article

MAGNETIC INTAKE LIMITATIONS ON INTERSTELLAR RAMJETS = LIMITATION D'ADMISSION MAGNETIQUE DANS LES STATOREACTEURS INTERSTELLAIRESMARTIN AR.1973; ASTRONAUT. ACTA; G.B.; DA. 1973; VOL. 18; NO 1; PP. 1-10; ABS. FR. ALLEMSerial Issue

INTEGRATED SCRAMJET NOZZLE/AFTERBODY PERFORMANCE ANALYSIS.SADUNAS JA.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 11; PP. 867-872; BIBL. 12 REF.Article

ETUDE THEORIQUE ET EXPERIMENTALE D'UN STATOREACTEUR A COMBUSTION MIXTE (DOMAINE DE VOL MACH 3,5/7CONTENSOU P; MARGUET R; HUET C et al.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 24; PP. 1-15; ABS. ANGL.; BIBL. 12 REF.Conference Paper

EXPERIMENTAL STUDY OF JET MIXING MECHANISMS IN A MODEL SECONDARY COMBUSTORISHIKAWA N.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 4; PP. 565-571; BIBL. 17 REF.Article

NUMERICAL STUDY OF A SCRAMJET ENGINE FLOWFIELDDRUMMOND JP; WEIDNER EH.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 9; PP. 1182-1187; BIBL. 16 REF.Article

STREAMTUBE ANALYSIS OF A HYDROGEN-BURNING SCRAMJET EXHAUST AND SIMULATION TECHNIQUE.TALCOTT NA JR; HUNT JL.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 9; PP. 918-920; BIBL. 7 REF.Article

SYSTEMATIC APPROACH TO AIR BREATHING MISSILE ENGINE CONTROLSPLANT AB.sdJOINT PROPULSION CONFERENCE. 16/1980/HARTFORD CT; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. S.D.; 9 P.; BIBL. 1 REF.Conference Paper

Avion spatial : la piste des réacteurs hypersoniques = Spacecraft: the track of the hypersonic ramjetJACKSON, Thomas.Pour la science. 2006, Num 348, pp 76-82, issn 0153-4092, 7 p.Article

FLAMMENSTABILISIERUNG IN STAUSTRAHL-BRENNKAMMERN DURCH EINEN PILOT-GASGENERATOR. = FLAME STABILIZATION IN A RAMJET COMBUSTOR BY MEANS OF A PILOT GAS GENERATOR = STABILISATION DE LA FLAMME, DANS LA CHAMBRE DE COMBUSTION D'UN STATOREACTEUR, A L'AIDE D'UN GENERATEUR DE GAZ PILOTERIESTER E.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 54; PP. 1-53; ABS. ANGL.; BIBL. 2 P.Serial Issue

A FLUIDIC FUEL CONTROL FOR ADVANCED RAMJET ENGINESCHAPIN DW; SCHEER LE; WALDON BE et al.sdJOINT PROPULSION CONFERENCE. 16/1980/HARTFORD CT; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. S.D.; 9 P.Conference Paper

RAMJETS AND RAMROCKETS FOR MILITARY APPLICATIONS. PAPERS PRESENTED AT THE PROPULSION AND ENERGETICS 58TH SYMPOSIUM HELD AT LONDON, UK ON 26-29 OCTOBER 19811982; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1982; NO 307; PAG. MULT.; BIBL. DISSEM.Conference Paper

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