| Citation: | ZHAO Hai-gang, SHEN Shi-cai, ZHANG Xiao-fei, MA Yan-rong, WANG Xiao-feng. Flight test of mass flow measurement of turbofan engine[J]. Journal of Aerospace Power, 2012, 27(8): 1778-1784.
|
| [1] |
Saravanmuttoo H I H.Recommended practice for measurement of gas path pressures and temperatures for performance assesment of air craft turbine engines and components .AGARD Advisory Report No.245,1990.
|
| [2] |
Trong T B,David L O.Design and evaluation of a new boundary-layer measurement rake for flight testing .NASA TM-2000-209014,2000.
|
| [3] |
Robert D Q,Leslie G.In-flight boundary-layer measurements on a hollow cylinder at Mach number of 3.0 .NASA TP-1980-1764,1980.
|
| [4] |
杨琳,邹正平,李维,等.尾迹作用下不同负荷分布叶型边界层发展研究[J].工程热物理学报,2006,27(5):751-753. YANG Lin,ZOU Zhengping,LI Wei,et al.Investigation of boundary layer developm ent for different loading distribution considering wake effect[J].Journal of Engineering Thermophysics,2006,27(5):751-753.(in Chinese)
|
| [5] |
杨海涛.低速压气机中CLOCKING效应的数值模拟 .哈尔滨:哈尔滨工业大学,2004. YANG Haitao.Numerical simulation of CLOCKING effect in a low speed compressor .Harbin:Harbin Institute of Technology,2004.(in Chinese)
|
| [6] |
侯安平,周盛.轴流式叶轮机时序效应的机理探讨[J].航空动力学报,2003,18(1):70-75. HOU Anping,ZHOU Sheng.Probe into the mechanism of docking effect in turbomachinery[J].Journal of Aerospace Power,2003,18(1):70-75.(in Chinese)
|
| [7] |
赵桂杰.弯掠扩压叶栅附面层流动控制的实验研究与数值模拟 .哈尔滨:哈尔滨工业大学,2005. ZHAO Guijie.Experimental and numerical study on the curved swept compressor cascade boundary layer flow control .Harbin:Harbin Institute of Technology,2005.(in Chinese)
|
| [8] |
Ottavy X,Vilmin S,Opoka M,et al.The effects of Wake passing unsteadiness over a highly-loaded compres Sot like flat plate .ASME Paper GT-2002-30354,2002.
|
| [9] |
Waiters D K,Leylek J H.A CFD study of wake-induced transition on a compressor-like flat plate .ASME Paper GT-2003-38680,2003.
|
| [10] |
刘波,王掩刚,肖敏.压气机叶栅叶片表面附面层流态变化影响因素探讨[J].推进技术,1999,20(3):64-68. LIU Bo,WANG Yangang,XIAO Min.Effect of inlet flow condition boundary flow on compressor blade surface[J].Journal of Propulsion Technology,1999,20(3):64-68.(in Chinese)
|
| [11] |
Mayle R E.The role of laminar-turbulent transition in gasturbine engines[J].ASME Journal of Turbomachinery,1991,113(4):509-537.
|
| [12] |
Keener E R,Spaid F W.Hypersonic nozzle-afterbody experiment:flow visualization and boundary-layer measurements[J].Journal of Spacecraft and Rockets,1996,33(3):326-332.
|
| [13] |
Bobby L B,Melissa B C,Brian G A.High Reynolds number investigation of a flush-mounted,S-duct inlet with large amounts of boundary layer ingestion .NASA TP-2005-213766,2005.
|
| [14] |
Murthy A V.Calculation of sidewall boundary-layer parameters from rake measurements for the langley 0.3 meter transonic cryogenic tunnel .NASA CP-1987-178241, 1987.
|
| [15] |
Beale D K,Cramer K B,King P S.Development of improved methods for simulating aircraft inlet distortion in turbine engine ground test .AIAA Paper 2002- 3045, 2002.
|
DownLoad: