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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

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

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

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

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

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

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

Experimental characterization of onset of acoustic instability in a nonpremixed half-dump combustorCHAKRAVARTHY, Satyanarayanan R; SHREENIVASAN, Obla J; BOEHM, Benjamin et al.The Journal of the Acoustical Society of America. 2007, Vol 122, Num 1, pp 120-127, issn 0001-4966, 8 p.Article

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

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

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

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

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

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

A mechanism of combustion mode transition for hydrogen fueled scramjetQINGCHUN YANG; JUNTAO CHANG; WEN BAO et al.International journal of hydrogen energy. 2014, Vol 39, Num 18, pp 9791-9797, issn 0360-3199, 7 p.Article

Closed-form model for three-dimensional vacuum plumes from a scarfed nozzleROMINE, G. L; NOBLE, J. A.AIAA journal. 1984, Vol 22, Num 5, pp 719-721, issn 0001-1452Article