Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector mode
暂无分享,去创建一个
Menglei Li | Peibo Li | Yuhui Huang | Ming-Chien Sun | Rui Gu | Dongdong Zhang | Yizhi Yao | Mingbo Sun | Yuhui Huang | Peibo Li | B. An | Taiyu Wang | Jikai Chen | Jiaoru Wang | Yizhi Yao | Dongdong Zhang | Jiao Wang
[1] A. Tounsi,et al. Predicting elemental stiffness matrix of FG nanoplates using Gaussian Process Regression based surrogate model in framework of layerwise model , 2022, Engineering Analysis with Boundary Elements.
[2] Peng Cui,et al. Mixing enhancement of supersonic flow induced by splitter plate cavity , 2022, Aerospace Science and Technology.
[3] Y. Egami,et al. Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity , 2021 .
[4] Jianguo Tan,et al. Vortex evolution and flame propagation driven by oblique shock wave in supersonic reactive mixing layer , 2021 .
[5] R. Yang,et al. Flows visualization for a supersonic mixing layer behind the blunt trailing edge under non-isobaric initial conditions , 2021, Thermophysics and Aeromechanics.
[6] B. R. Noack. Machine learning open-loop control of a mixing layer , 2020 .
[7] Zhenguo Wang,et al. Numerical investigation on flow and mixing characteristics inside a converging-diverging mixing duct of rocket-based combined-cycle engine in ejector mode , 2020 .
[8] Qiang Li,et al. Numerical and experimental investigation of the geometrical scale effect on a confined subsonic-supersonic shear layer , 2020 .
[9] Peijin Liu,et al. Mixing enhancement in a subsonic-supersonic shear layer with a cavity splitter plate , 2020 .
[10] Jiang Li,et al. Experimental study on evolution characteristics of plane subsonic-supersonic shear layer , 2020 .
[11] Aytac Altan,et al. Model predictive control of three-axis gimbal system mounted on UAV for real-time target tracking under external disturbances , 2020 .
[12] Yun Wu,et al. Shock-Wave/Boundary-Layer Interactions at Compression Ramps Studied by High-Speed Schlieren , 2020 .
[13] Zhenguo Wang,et al. Characteristics of laser ignition and spark discharge ignition in a cavity-based supersonic combustor , 2020 .
[14] Ruiying Li,et al. Artificial intelligence control of a turbulent jet , 2018, Journal of Fluid Mechanics.
[15] Liu Yang,et al. Direct numerical simulation of fine flow structures of subsonic-supersonic mixing layer , 2019 .
[16] Zun Cai,et al. Survey on key techniques of rocket-based combined-cycle engine in ejector mode , 2019, Acta Astronautica.
[17] Ye Wei,et al. Climbing performance analysis of rocket-based combined cycle engine powered aircraft , 2019, Acta Astronautica.
[18] Stephen B. Jones,et al. Unsteady Analysis of Shock-Wave/Boundary-Layer Interaction Experiments at Mach 4.2 , 2019, AIAA Journal.
[19] Fei Qin,et al. Research progress on ejector mode of rocket-based combined-cycle engines , 2019, Progress in Aerospace Sciences.
[20] Jianguo Tan,et al. Direct numerical simulation of spatially developing highly compressible mixing layer: Structural evolution and turbulent statistics , 2019, Physics of Fluids.
[21] Srisha M. V. Rao,et al. Effect of shock interactions on mixing layer between co-flowing supersonic flows in a confined duct , 2018 .
[22] Jie Liu,et al. A rocket-based combined-cycle engine prototype demonstrating comprehensive component compatibility and effective mode transition , 2016 .
[23] Wen Bao,et al. Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine , 2015 .
[24] B. Wang,et al. Mixing Enhancement of Compressible Planar Mixing Layer Impinged by Oblique Shock Waves , 2015 .
[25] Li Yan,et al. Survey on the mode transition technique in combined cycle propulsion systems , 2014 .
[26] Bin Chen,et al. Design and Optimization of RBCC Powered Suborbital Reusable Launch Vehicle , 2014 .
[27] Chaoqun Liu,et al. Study on shock wave-vortex ring interaction by the micro vortex generator controlled ramp flow with turbulent inflow , 2013 .
[28] Hossein Zare-Behtash,et al. Effect of primary jet geometry on ejector performance: A cold-flow investigation , 2011 .
[29] Ajay P. Kothari,et al. A Reusable, Rocket and Airbreathing Combined Cycle Hypersonic Vehicle Design for Access-to-Space , 2010 .
[30] Gopalan Jagadeesh,et al. Study of Detonation Interactions Inside a Two-Dimensional Ejector Using Detonation Transmission Tubing , 2010 .
[31] Hossein Zare-Behtash,et al. Compressible Flow Structures Interaction with a Two-Dimensional Ejector: A Cold-Flow Study , 2009 .
[32] Kouichiro Tani,et al. Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane , 2007 .
[33] Tetsuo Hiraiwa,et al. Recent progress in scramjet/combined cycle engines at JAXA, Kakuda space center , 2006 .
[34] Jean P. Sislian,et al. Effect of rocket exhaust configurations on ejector performance in RBCC engines , 2005 .
[35] Ronald S. Fry,et al. A Century of Ramjet Propulsion Technology Evolution , 2004 .
[36] Takeshi Kanda,et al. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane , 2003 .
[37] R. Cummings,et al. Fifty years of hypersonics: where we've been, where we're going , 2003 .
[38] John R. Olds,et al. SCCREAM: A Conceptual Rocket-Based Combined-Cycle Engine Performance Analysis Tool , 2001 .
[39] B. Cetegen,et al. Shock-induced mixing of nonhomogeneous density turbulent jets , 2000 .
[40] J Craig Dutton,et al. PLANAR VISUALIZATIONS OF LARGE-SCALE TURBULENT STRUCTURES IN AXISYMMETRIC SUPERSONIC SEPARATED FLOWS , 1999 .
[41] J. C. Dutton,et al. Investigation of Large-Scale Structures in Supersonic Planar Base Flows , 1996 .
[42] Walter R. Lempert,et al. Two-dimensional measurement of density, velocity, and temperature in turbulent high-speed air flows by UV rayleigh scattering , 1990 .
[43] William J. D. Escher,et al. Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered single-stage-to-orbit (SSTO) vehicle , 1989 .
[44] Neil D. Sandham,et al. Compressible mixing layer - Linear theory and direct simulation , 1989 .
[45] Dimitri Papamoschou,et al. STRUCTURE OF THE COMPRESSIBLE TURBULENT SHEAR LAYER , 1989 .
[46] A. Roshko,et al. The compressible turbulent shear layer: an experimental study , 1988, Journal of Fluid Mechanics.
[47] A. Kerstein,et al. Alignment of vorticity and scalar gradient with strain rate in simulated Navier-Stokes turbulence , 1987 .
[48] D. W. Bogdanoff,et al. Compressibility Effects in Turbulent Shear Layers , 1983 .
[49] A. Roshko,et al. On density effects and large structure in turbulent mixing layers , 1974, Journal of Fluid Mechanics.