| Citation: | LIU Bo, WANG Lei, HUANG Jian. Further validation of NHM in two-stage counter-rotating compressor[J]. Journal of Aerospace Power, 2013, 28(6): 1333-1341.
|
| [1] |
He L.Method of simulating unsteady turbomachinery flows with multiple perturbations[J].AIAA Journal,1992,30(11):2730-2735.
|
| [2] |
Srivastava R,Bakhle M,Keith T G.Numerical simulation of aerodynamic damping for flutter analysis of turbomachinery blade rows[J].Journal of Propulsion and Power,2003,19(2):60-267.
|
| [3] |
Bakhle M,Thomas J,Reddy T.Fan flutter computations using the harmonic balance method.AIAA-2008-4743,2008.
|
| [4] |
He L,Chen T,Wells R G,et al.Analysis of rotor-rotor and stator-stator interferences in multi-stage turbomachines[J].Journal of Turbomachinery,2002,124(4):564-571.
|
| [5] |
Ning W,He L.Some modeling issues on trailing-edge vortex shedding[J].AIAA Journal,2001,39(5):787-793.
|
| [6] |
He L,Li Y S,Wells R G.Predicting bladerow interactions using a multistage time-linearized Navier-Stokes solver[J].Journal of Turbomachinery,2003,25(1):25-32.
|
| [7] |
Van der Weide E,Gopinath G,Jameson A.Turbomachinery applications with the time spectral method[R].AIAA-2005-4905,2005.
|
| [8] |
Im D K,Kwon J H,Park S H.Periodic unsteady flow analysis using a diagonally implicit harmonic balance method[J].AIAA Journal,2012,50(3):741-745.
|
| [9] |
Kwon H I,Yi S G,Im D K.Design of a low-noise open rotor using an implicit harmonic balance method[R].AIAA-2013-1090,2013.
|
| [10] |
Sicot F,Hassan D.A time-domain harmonic balance method for dynamic derivatives predictions[R].AIAA-2011-1242,2011.
|
| [11] |
赵军,柳阳威,刘宝杰.NASA67级非定常流场的频域分析[J].航空动力学报,2007,22(8):1371-1377. ZHAO Jun,LIU Yangwei,LIU Baojie.Frequency-domain analysis of NASA67 unsteady flow field[J].Journal of Aerospace Power,2007,22(8):1371-1377.(in Chinese)
|
| [12] |
Wang L,Liu B,Xiang X R,et al.Investigtion of the unsteady flow in a counter-rotating compresor using the nonlinear harmonic method[R].ISABE Paper-2011-1234,2011.
|
| [13] |
Hall E J.Aerodynamic modeling of multistage compressor flow fields:Part 2 modeling deterministic stresses[J].Journal of Aerospace Engineering,1998,212(2):91-107.
|
| [14] |
He L.Fourier modeling of steady and unsteady nonaxisymmetrical flows[J].Journal of Propulsion and Power,2006,22(2):197-201.
|
| [15] |
王雷,刘波.非线性谐波法在对转压气机中的校检分析[J].航空动力学报,2012,27(7):1448-1455. WANG Lei,LIU Bo.Validaton of nonlinear harmonic method in dual-stage counter-rotating compressor[J].Journal of Aerospace Power,2007,22(8):1371-1377.(in Chinese)
|
| [16] |
Chen Y Y,Liu B,Xuan Y,et al.A study of speed ratio affecting the performance of a contra-rotating axial compressor[J].Journal of Aerospace Engineering,2008,222(7):985-991.
|
| [17] |
He L.On circumferential phase-shift condition for turbomachinery aerodynamic and aeromechanical applications[R].AIAA-2005-0016,2005.
|
| [18] |
Hembera M,Loos A,Kau H P,et al.Comparing a 40 Mio gridpoints full-annulus computation with a 7 Mio gridpoints nonlinear harmonic computation[R].AIAA-2009-930,2009.
|
| [19] |
柳阳威,刘宝杰.跨音压气机确定应力场分析[J].航空学报,2007,28(增刊):1-6. LIU Yangwei,LIU Baojie.Analysis of deterministic stresses in a transonic compressor[J].Acta Aeronautica et Astronautica Sinica,2007,28(Sup.):1-6.(in Chinese)
|
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