XIE Yi， ZHONG Chen， RUAN Deng-fang， LIU Kun. Combustion Characteristics of Micro-lobed Burner[J]. Journal of Northeastern University Natural Science, 2017, 38(4): 536-541.
[1]Epstein A H，Senturia S D，Al-Midani O，et al.Micro-heat engines，gas turbines，and rocket engines—the MIT microengine project［C］//The 28th Fluid Dynamics Conference.Snowmass Village，1997:1-7. [2]Epstein A H，Senturia S D，Anathasuresh G，et al.Power MEMS and microengines［C］// The 9th International Conference on Solid-State Sensors and Actuators，Transducers.Chicago，1997:753-756. [3]Isomura K，Tanaka S，Togo S I，et al.Development of high-speed micro-gas bearings for three-dimensional micro-turbo machines［J］.Journal of Micromechanics and Microengineering，2005，15(9):222-227. [4]Paterson R W.Turbofan mixer nozzle flow of an mixer nozzle flow field—a benchmark experimental study［J］.Journal of Engineering for Gas Turbines and Power，1984，106(3):692-698. [5]Skebe S A，Paterson R W，Baber T J.Experimental investigation of three-dimensional forced mixer lobe flow field［C］// The 1st National Fluid Dynamics Conference.Cincinnati，1988:1999-2006. [6]Presz W M，Reynolds G，Mccormick D C.Thrust augmentation using mixer ejector diffuser systems［C］//Aerospace Sciences Meeting and Exhibit.Reno，1994:1-10. [7]Presz W M.Mixer/ejector noise suppressors［C］// The 27th Joint Propulsion Conference.Sacramento，1991:1-10. [8]Cooper N J，Merati P，Hu H.Numerical simulation of the vertical structures in a lobed jet mixing flow［C］// The 43rd AIAA Aerospace Sciences Meeting and Exhibit.Reno，2005:1-13. [9]Andrew T T，Christopher K W.Computation of turbulent axisymmetric and nonaxisymmetric jet flows using the k-ε model［J］.AIAA Journal，1996，34(2):309-316.
