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

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

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

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

PENETRATION AND BREAKUP OF SLURRY JETS IN A SUPERSONIC STREAMLESS DM; SCHETZ JA.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 7; PP. 1045-1048; BIBL. 6 REF.Article

Etude des instabilités de combustion dans les statoréacteurs = Study of combustion instabilities in ramjetsSamaniego, Jean-Michel; Poinsot, Thierry.1992, 242 p.Thesis

Optimal return-to-base cruise of hypersonic carrier vehiclesBAYER, R; SACHS, G.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1995, Vol 19, Num 1, pp 47-54, issn 0342-068XArticle

Efficiency analysis of reusable aerospace launchersLOBANOVSKY, YU. I.Aerospace science and technology. 1997, Vol 1, Num 1, pp 37-46, issn 1270-9638Article

Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjetQINGCHUN YANG; JUNTAO CHANG; WEN BAO et al.Energy (Oxford). 2014, Vol 76, pp 552-558, issn 0360-5442, 7 p.Article

Burning rate characteristics of solid fuels for an un-choked solid fuel ramjetNAKAGAWA, I; KUWAHARA, T; KONO, M et al.Kayaku Gakkaishi. 1994, Vol 55, Num 6, pp 243-250, issn 1340-2781Article

The A/F self modulation function and the burning rate characteristics of the fuel of an un-chocked solid fuel ramjetNAKAGAWA, I; KUWAHARA, T.Kayaku Gakkaishi. 1996, Vol 57, Num 4, pp 142-147, issn 1340-2781Article