| Citation: | Numerical simulation and experiment of laminar separation bubble transition and corner separation of compressor stator cascade[J]. Journal of Aerospace Power, 2017, 32(9): 2273-2282. doi: 10.13224/j.cnki.jasp.2017.09.028
|
| [1] |
SCHREIBER H A,STEINERT W,KSTERS B. Effects of Reynolds number and freestream turbulence on boundary layer transition in a compressor cascade[J].Journal of Turbomachinery,2002,124(1):1-9.
|
| [2] |
杨琳,邹正平,宁方飞,等.边界层转捩的数值模拟[J].航空动力学报,2005,20(3):355-360. YANG Lin,ZHOU Zhengping,NING Fangfei,et al.Numerical study of the boundary layer transition[J].Journal of Aerospace Power,2005,20(3):355-360.(in Chinese)
|
| [3] |
DONG Y,CUMPSTY N A.Compressor blade boundary layers:Part 2 measurements with incident wakes[J].Journal of Turbomachinery,1990,112(2):231-240.
|
| [4] |
TEUSCH R,FOTTNER L,SWOBODA M.Experimental investigation of wakeinduced transition in a linear compressor cascade with controlled diffusion balding[R].Florence,Italy:International Society for Air Breathing Engines,1999.
|
| [5] |
SOLOMON W J,WALKER G J.Observations of wakeinduced transition on an axial compressor blade[R].ASME Paper 95-GT-381,1995.
|
| [6] |
HALSTEAD D E,WISLER D C,OKIISHI T H,et al.Boundary layer development in axial compressors and turbines:Part 1 of 4 composite picture[R].ASME Paper 95-GT-461,1995.
|
| [7] |
MENTER F R,LANGTRY R B,LIKKI S R,et al.A correlationbased transition model using local variables:Part Ⅰ model formulation[J].Journal of Turbomachinery,2006,128(3):413-422.
|
| [8] |
LANGTRY R B,MENTER F R,LIKKI S R,et al.A correlationbased transition model using local variables:Part Ⅱ test cases and industrial applications[J].Journal of Turbomachinery,2006,128(3):423-434.
|
| [9] |
ZHANG Y,MAHALLATI A,BENNER M.Experimental and numerical investigation of corner stall in a highlyloaded compressor cascade[R].ASME Paper GT2014-27204,2014.
|
| [10] |
MINOT A,DE SAINTVICTOR X,MARTY J,et al.Advanced numerical setup for separationinduced transition on highlift lowpressure turbine flows using the γ-Rθt model[R].ASME Paper GT2015-42160,2015.
|
| [11] |
WISLER D C.Loss reduction in axialflow compressors through lowspeed model testing[J].Journal of Engineering for Gas Turbines and Power,1985,107(2):354-363.
|
| [12] |
王丹华,陆利蓬,李秋实.基于湍流输运特性对SA模型在压气机角区流动模拟中的改进研究[J].航空动力学报,2010,25(1):80-86. WANG Danhua,LU Lipeng,LI Qiushi.Research on improvement of SA model in the simulation of compressor corner flow based on the turbulence transport properties[J].Journal of Aerospace Power,2010,25(1):80-86.(in Chinese)
|
| [13] |
JOSLYN H D,DRING R P.Axial compressor stator aerodynamics[J].Journal of Engineering for Gas Turbines and Power,1985,107(2):485-492.
|
| [14] |
GBADEBO S A,CUMPSTY N A,HYNES T P.Threedimensional separations in axial compressors[R].Journal of Turbomachinery,2004,127(2):331-339.
|
| [15] |
LEWIN E,KOULOVIC＇ D,STARK U.Experimental and numerical analysis of hubcorner stall in compressor cascades[R].Glasgow,UK：ASME Turbo Expo,2010.
|
| [16] |
MA W,OTTAVY X,LU L,et al.Experimental investigations of corner stall in a linear compressor cascade[R].Chinese Journal of Aeronautics,2011,24(3):235-242.
|
| [17] |
WANG Z N,YUAN X.Unsteady mechanisms of compressor corner separation over a range of incidences based on hybrid LES/RANS[R].ASME Paper GT2013-95300,2013.
|
| [18] |
王子楠,高磊,耿少娟,等.不同端壁间隙下压气机平面叶栅角区流动的数值模拟和实验研究[J].工程热物理学报,2015 (7):1428-1432. WANG Zinan,GAO Lei,GENG Shaojuan,et al.Numerical and experimental study for corner flow of a compressor linear cascade with different sizes of endwall clearance[J].Journal of Engineering Thermophysics,2015.(in Chinese)
|
DownLoad: