1. JacksonT.A.PowerforaSpacePlane.ScientificAmerican.(alsoinNIKKEIScience,(2006)pp.98-107.Nobember 2006.) 2.NaitohK,Engine.Submittedaspatents(2010,2011,2012). 3.NaitohK,NakamuraK.,EmotoT.ANewCascade-LessEngineOperatedfromSubsonictoHypersonicConditions. J. of ThermalScience,19-6, (2010)pp.481-485.4.Naitoh K.Nakamura K., Emoto T., A Wide-range single engine: operated from startup to hypersonic.AIAA paper2011-2316, (2011) .5.Naitoh K., NakamuraK., Emoto T.,Kainuma Y.Wide-range Single Engine:Operated from Subsonic to Hypersonic Conditions Designedby ComputationalFluidDynamics.SAE paper 2011-01-2027. (2011).6.Naitoh K., Shimizu D., Nonaka S., Kainuma Y.and Emoto T. The Fifthcompression strategy for hypersonic aircar:proposedby three experiments ofshock-tube, computation, andthought.AIAApaper-2012-3314, 2012.7.Naitoh K., Tanaka S., Emoto T., Kainuma Y., Kurihara M, Shimizu D., Nonaka S., Iseno M., Kubota T., Hashimoto S. Supermulti-jets colliding for realizing the ultimate engine: proposed by shocktube analysis, computation, andtheoretical thought.Proceedings of COMODIA2012, 2012.8.LandauE.D.andLifshitzE.M.Fluidmechanics.2ndEdition,(Butterworth-HeinemannElsevier,Oxford2004).9.Takewaki H, Nishiguchi A, and Yabe T.The Cubic-Interpolated Pseudo-Particle (CIP) Method for Sorving Hyperbolic-TypeEquations", J.Comput. Phys.Vol. 61, (1985) p.261.10.Naitoh K and Kuwahara K. Large eddy simulation and direct simulation of compressible turbulence and combusting flows inengines based on the BI-SCALES method,Fluid Dynamics Research10, (1992) pp.299-325.11.Naitoh K., Nakagawa Y., and Shimiya H. Stochastic determinism approach for simulating the transition points in internal flows with various inlet disturbances. Proc. of ICCFD5, Computational Fluid Dynamics 2008, Springer-Verlag.(2008)12.Naitoh K. and ShimiyaH.Stochastic determinism capturing the transition point from laminar flow to turbulence. Japan Journal of Industrial and Applied Mathematics, (2011). [Also in Proc. of 6th Int. Symposium on Turbulence and Shear Flow Phenomena (TSFP6), 2009].13.Korobeinikov V.P., Propagation of Blast Waves in a Combustible GasAstronamicaActa Vol.17 pp.529-537 (1972)14.Asanuma T, Obokata T., and Nagashima T. Experimental Study on Supersonic Air Intake Buzz. Bulletin of the Institute ofSpace and Aeronautical Science, University ofTokyo, 9(2_C), (1973) pp. 499-542.15.Kailasanath,K.,ReviewofPropulsionApplicationsofDetonationWaves,AIAAJournal,Vol.39,No.9,(2000)pp. 1698-1708.