Title: Parametric Scramjet Cycle Analysis for Nonideal Mass Flow Rate
Abstract: No AccessTechnical NoteParametric Scramjet Cycle Analysis for Nonideal Mass Flow RateJ. A. Roux, J. Choi and N. ShakyaJ. A. RouxDepartment of Mechanical Engineering, University of Mississippi, University, Mississippi 38677*Professor, Department of Mechanical Engineering. Associate Fellow AIAA.Search for more papers by this author, J. ChoiDepartment of Mechanical Engineering, University of Mississippi, University, Mississippi 38677†Graduate Student.Search for more papers by this author and N. ShakyaDepartment of Mechanical Engineering, University of Mississippi, University, Mississippi 38677†Graduate Student.Search for more papers by this authorPublished Online:30 Jan 2014https://doi.org/10.2514/1.T4217SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Roux J. A., Shakya N. and Choi J., “Revised Parametric Ideal Scramjet Cycle Analysis,” Journal of Thermophysics and Heat Transfer, Vol. 27, No. 1, 2013, pp. 178–183. doi:https://doi.org/10.2514/1.T3961 JTHTEO 0887-8722 LinkGoogle Scholar[2] Mattingly J. D. and Ohain H., Elements of Propulsion: Gas Turbines and Rockets, AIAA Education Series, AIAA, Reston, VA, 2006, pp. 266–277. LinkGoogle Scholar[3] Hill P. G. and Peterson C. R., Mechanics and Thermodynamics of Propulsion, 2nd ed., Addison Wesley Longman, Reading, MA, 1992, pp. 155–164. Google Scholar[4] Smart M. K., Hass N. E. and Paull A., “Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment,” AIAA Journal, Vol. 44, No. 10, 2006, pp. 2366–2375. doi:https://doi.org/10.2514/1.20661 AIAJAH 0001-1452 LinkGoogle Scholar[5] Lewis M., “X-51 Scrams into the Future,” Aerospace America, Vol. 48, No. 9, Oct. 2010, pp. 26–31. AEAME2 0740-722X Google Scholar[6] Dora M., “High-Speed Air-Breathing Propulsion,” Aerospace America, Vol. 48, No. 11, Dec. 2010, p. 57. AEAME2 0740-722X Google Scholar[7] Curran E. T. and Murthy S. N. B., Scramjet Propulsion, edited by Zarchan P., Vol. 189, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000, pp. 369–414. Google Scholar[8] Segal C., The Scramjet Engine, Processes and Characteristics, Cambridge Univ. Press, New York, 2009, pp. 62–68. CrossrefGoogle Scholar[9] Prisell E. G., “The Feasibility of the Scramjet: An Analysis Based on First Principles,” Proceedings of the 25th International Congress of the Aeronautical Sciences, ICAS, Hamburg, Germany, 2006, pp. 1–14. Google Scholar[10] Cengel Y. A. and Boles M. A., Thermodynamics: An Engineering Approach, 3rd ed., McGraw–Hill, New York, 1998, pp. 472–477. Google Scholar[11] Roux J. A., “Optimum Freestream Mach Number for Maximum Thrust Flux for Ideal Ramjet/Scramjet,” Journal of Thermophysics and Heat Transfer, Vol. 26, No. 2, 2012, pp. 390–392. doi:https://doi.org/10.2514/1.T3845 JTHTEO 0887-8722 CrossrefGoogle Scholar Previous article
Publication Year: 2014
Publication Date: 2014-01-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 8
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