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- W2112979713 abstract "No AccessTechnical NotePerformance Analysis of a Mach 12 Scramjet at Off-Design ConditionsY. Moule and M. K. SmartY. MouleCentre for Hypersonics, University of Queensland, Brisbane, Queensland 4072, Australia*Research Assistant, Centre for Hypersonics; currently Ph.D. Candidate, Onera, The French Aerospace Laboratory, F-91761 Palaiseau, France.Search for more papers by this author and M. K. SmartCentre for Hypersonics, University of Queensland, Brisbane, Queensland 4072, Australia†Professor, Centre for Hypersonics. Senior Member AIAA.Search for more papers by this authorPublished Online:28 Jan 2013https://doi.org/10.2514/1.B34563SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Vinogradov V. A., Shikman Y. M. and Segal C., “A Review of Fuel Pre-Injection in Supersonic, Chemically Reacting Flows,” ASME Applied Mechanics Reviews, Vol. 60, No. 4, 2007, pp. 139–148.doi:https://doi.org/10.1115/1.2750346 CrossrefGoogle Scholar[2] Turner J. C. and Smart M. K., “Application of Inlet Injection to a 3-D Scramjet at Mach 8,” AIAA Journal, Vol. 48, No. 4, 2010, pp. 829–838. doi:https://doi.org/10.2514/1.J050052 AIAJAH 0001-1452 LinkGoogle Scholar[3] Stalker R. J., “Control of Hypersonic Turbulent Skin Friction by Boundary-Layer Combustion of Hydrogen,” Journal of Spacecraft and Rockets, Vol. 42, No. 4, 2005, pp. 577–587. doi:https://doi.org/10.2514/1.8699 JSCRAG 0022-4650 LinkGoogle Scholar[4] Suraweera M. V. and Smart M. K., “Shock Tunnel Experiments with a Mach 12 Rectangular-to-Elliptical Transition Scramjet at Off-Design Conditions,” Journal of Propulsion and Power, Vol. 25, No. 3, 2009, pp. 555–564. doi:https://doi.org/10.2514/1.37946 JPPOEL 0748-4658 LinkGoogle Scholar[5] Smart M. K., “Scramjets,” Aeronautical Journal, Vol. 111, No. 1124, 2007, pp. 605–620. CrossrefGoogle Scholar[6] Heiser W. H. and Pratt D. T., Hypersonic Airbreathing Propulsion, AIAA Educational Series, AIAA, Washington, DC, 1994, pp. 149–197. LinkGoogle Scholar[7] White J. A. and Morrison J. H., “A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier–Stokes Equations,” 14th AIAA Computational Fluid Dynamics Conference, AIAA Paper 1999-3360, 1999. LinkGoogle Scholar Previous article Next article" @default.
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- W2112979713 title "Performance Analysis of a Mach 12 Scramjet at Off-Design Conditions" @default.
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