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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

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

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

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

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

Low-frequency combustion oscillations in a model afterburnerMACQUISTEN, M. A; DOWLING, A. P.Combustion and flame. 1993, Vol 94, Num 3, pp 253-264, issn 0010-2180Article

calculation of supersonic turbulent reacting coaxial jetsEKLUND, D. R; DRUMMOND, J. P; HASSAN, H. A et al.AIAA journal. 1990, Vol 28, Num 9, pp 1633-1641, issn 0001-1452, 9 p.Article

Sui problemi tecnologici e scientifici della combustione supersonica = Problèmes technologiques et scientifiques de la combustion supersonique = Technological and scientific problems of supersonic combustionCASCI, C.Rivista dei Combustibili. 1989, Vol 43, Num 4, pp 129-150, issn 0370-5463Article

Numerical study on supersonic combustion with cavity-based fuel injectionKIM, Kyung Moo; SEUNG WOOK BAEK; CHO YOUNG HAN et al.International journal of heat and mass transfer. 2004, Vol 47, Num 2, pp 271-286, issn 0017-9310, 16 p.Article

Computational modeling of high pressure combustion mechanism in scram acceleratorCHOI, J.-Y; LEE, B.-J; JEUNG, I.-S et al.Journal de physique. IV. 2000, Vol 10, Num 11, pp Pr11.131-Pr11.141, issn 1155-4339Conference Paper

Pulsed detonation engine. Numerical studySELLAM, M; FORESTIER, A. J.Journal de physique. IV. 2000, Vol 10, Num 11, pp Pr11.165-Pr11.174, issn 1155-4339Conference Paper

Chemical kinetics and self-ignition in a model supersonic hydrogen-air combustorSUNG, C. J; LI, J. G; YU, G et al.AIAA journal. 1999, Vol 37, Num 2, pp 208-214, issn 0001-1452Conference Paper

Quasiglobal reaction model for ethylene combustionSINGH, D. J; JACHIMOWSKI, C. J.AIAA journal. 1994, Vol 32, Num 1, pp 213-216, issn 0001-1452Article

Optimum Freestream Mach Number for Maximum Thrust Flux for Ideal Ramjet/ScramjetROUX, J. A.Journal of thermophysics and heat transfer. 2012, Vol 26, Num 2, pp 390-392, issn 0887-8722, 3 p.Article

Ideal Ramjet: Optimum Freestream Mach Number for Minimum Thrust-Specific Fuel ConsumptionROUX, J. A.Journal of thermophysics and heat transfer. 2011, Vol 25, Num 4, pp 626-627, issn 0887-8722, 2 p.Article

An expansion-Ludwieg tube for accelerating combustible gas mixtures to superdetonative speedsSRULIJES, J; SMEETS, G; PATZ, G et al.Journal de physique. IV. 2000, Vol 10, Num 11, pp Pr11.69-Pr11.77, issn 1155-4339Conference Paper

Ranking based uncertainty quantification for a multifidelity design approachUMAKANT, J; SUDHAKAR, K; MUJUMDAR, P. M et al.Journal of aircraft. 2007, Vol 44, Num 2, pp 410-419, issn 0021-8669, 10 p.Article

Inlet air temperature effects on the performance of the solid fuel ramjetLEE, Tae-Ho.Journal of thermophysics and heat transfer. 2006, Vol 20, Num 4, pp 937-939, issn 0887-8722, 3 p.Conference Paper

Enhanced RAMAC performance in subdetonative propulsion mode with semi-combustible projectileLEGENDRE, J.-F; GIRAUD, M.Journal de physique. IV. 2000, Vol 10, Num 11, pp Pr11.23-Pr11.30, issn 1155-4339Conference Paper

Optimization of Scramjet engin performance with the three-temperature flow modelTSUJIKAWA, Y; NORTHAM, G. B.International journal of hydrogen energy. 1995, Vol 20, Num 7, pp 593-599, issn 0360-3199Article

Modeling scramjet combustor flowfields with a grid adaptation schemeRAMAKRISHNAN, R; SINGH, D. J.AIAA journal. 1994, Vol 32, Num 5, pp 930-935, issn 0001-1452Article

Integrated vehicle comparison of turbo-ramjet engine and pulsed detonation engineKAEMMING, T.Journal of engineering for gas turbines and power. 2003, Vol 125, Num 1, pp 257-262, issn 0742-4795, 6 p.Conference Paper

Profiling of a supersonic combustion chamber and nozzle under constraints on the total lengthKRAIKO, A. N; MAKAROV, V. E; TILLYAYEVA, N. I et al.Fluid dynamics. 1998, Vol 33, Num 5, pp 637-644, issn 0015-4628Article

Fuel regression mechanism in a solid fuel ramjetHADAR, I; GANY, A.Propellants, explosives, pyrotechnics. 1992, Vol 17, Num 2, pp 70-76, issn 0721-3115Article

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