Browse by all authors Browse By Author ID - James Turner

Browse Results (6 results found)

Subscribe to the RSS feed for this result setSubscribe to the RSS feed for this result set

Refine

  Abstract Views File Downloads Thomson Reuters Web of Science Citation Count Scopus Citation Count Altmetric Score
Turner, J. C. and Smart, M. K. (2010) Application of inlet injection to a three-dimensional Scramjet at Mach 8. AIAA JOURNAL, 48 4: 829-838. doi:10.2514/1.J050052 81   9 Cited 18 times in Scopus18 0
Turner, James C. and Smart, Michael K. (2008). Application of radical farming to a 3-D scramjet at Mach 8. In: 2008 AIAA Meeting Papers on Disc. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, U.S.A, (). 7-10 January, 2008. 104   Cited 0 times in Scopus0
Chan, W. Y. K., Mee, D. J., Smart, M. K., Turner, J. C. and Stalker, R. J. (2010). Boundary layer combustion for viscous drag reduction in practical scramjet configurations. In: I. Grant, 27th International Congress of The Aeronautical Sciences (ICAS 2010), Nice, France, (1-10). 19-24 September 2010. 118 8
Wilson Chan, Mee, David J., Smart, Michael K. and Turner, James J. (2012). Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion. In: Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, (1-16). 24-28 September 2012. doi:10.2514/6.2012-5889 64 1 Cited 0 times in Scopus0 0
Turner, J. C. and Smart, M. K. (2009). Experimental investigation of inlet injection in a scramjet with rectangular to elliptical shape transition. In: Klaus Hannemann and Friedrich Seiler, Shock Waves: 26th International Symposium on Shock Waves, Volume 2. 26th International Symposium on Shock Waves (ISSW26), Deutsches Theater, Gottingen, Germany, (1117-1122). 15-20 July 2007. doi:10.1007/978-3-540-85181-3_52 125   0 0
Turner, James C. and Smart, Michael K. (2013) Mode change characteristics of a three-dimensional scramjet at mach 8. Journal of Propulsion and Power, 29 4: 982-990. doi:10.2514/1.B34569 42   3 Cited 4 times in Scopus4 0