[1] Qiao W Y. Aero-engine aeroacousitcs[M]. Beijing: Beihang University Press, 2010: 1-8. (in Chinese) 乔渭阳. 航空发动机气动声学[M]. 北京: 北京航空航天大学出版社, 2010: 1-8.[2] Heidmann M F. Interim prediction method for fan and compressor source noise, NASA TM X-71763[R]. Washington, D.C.: NASA, 1975.[3] Kontos K B, Janardan B A, Gliebe P R. Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion system. Volume 1: ANOPP evaluation and fan noise model improvement, NASA CR 195480[R]. Washington, D.C.: NASA, 1996.[4] Hough J W, Weir D S. Aircraft noise prediction program (ANOPP) fan noise prediction for small engines, NASA CR 198300[R]. Washington, D.C.: NASA, 1996.[5] Smith M J T, Bushell K W. Turbine noise -its signification in the civil aircraft noise problem, No.69-WA/GT-12[C]//ASME, 1969.[6] Dunn D G, Peart N A. Aircraft noise source and contour estimation, NASA CR-114649[R]. Washington, D.C.: NASA, 1973.[7] Matta R K, Sandusky G T, Doyle V L. GE core engine noise investigation-low emission engine, FAA-RD-77-4, AD A048590[R]. Cincinnati: Aircraft Engine Group, General Electric Company, 1977.[8] Ventres C S. Turbofan noise generation. Volume 2: computer programs, NASA CR-167952[R]. Washington, D.C.: NASA, 1983.[9] Ventres C S. Turbofan noise generation. Volume 1: analysis, NASA CR-167952[R]. Washington, D.C.: NASA, 1983.[10] Meyer H D, Envia E. Aeroacoustic analysis of turbofan noise generation, NASA CR-4715[R]. Washington, D.C.: NASA, 1996.[11] Montgomery M D. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows, NASA CR-4770[R]. Washington, D.C.: NASA, 1997.[12] Sawyer S, Nallasamy M, Hixonet R. Computational aeroacoustic prediction of discrete-frequency noise generated by a rotor-stator interaction[C]//9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003: 12-14.[13] Elhadidi B, Atassi H M. Passive noise control by blade lean and sweep[C]//10th AIAA/CEAS Aeroaoustics Conference, 2004: 10-12.[14] Tam C K W. Computational aeroacoustics: an overview of computational challenges and applications[J]. International Journal of Computational Fluid Dynamics, 2004, 18(6): 547-567.[15] Naoki T, Yoshiya N. Fan noise prediction using unsteady CFD analysis[C]//8th AIAA/CEAS Aeroacoustics Conference & Exhibit, 2002.[16] Tsuchiya N, Nakamura Y, Yamagata A, et al. Investigation of acoustic modes generated by rotor-stator interaction[C]//9th AIAA/CEAS Aero-acoustics Conference, 2003.[17] Keisuke T, Nobuhiko Y. Improved hybrid prediction of fan noise[C]//15th AIAA/CEAS Aeroacoustics Conference, 2009.[18] Polacsek C, Burguburu S, Redonnetet C. Numerical simulations of fan interaction noise using a hybrid approach[C]//11th AIAA/CEAS Aeroacoustics Conference, 2005.[19] WeckmÜeller C, Guerin S, Ashcroft G. CFD-CAA coupling applied to DLR UHBR-fan: comparison to experimental data[C]//15th AIAA/CEAS Aeroacoustics Conference, 2009.[20] Lebrun M, Favre C H. Fan-OGV unsteady Navier-Stokes computation using an adapted acoustic mesh[C]//10th AIAA/CEAS Aeroacoustics Conference, 2004.[21] Ovenden N C, Rienstra S W. In-duct matching stragies[M]. Eindhoven: Eindhoven University of Technology, 2002: 4-8.[22] Zhao L. Theory and method investigation of the aerodynamic-acoustics integration design in turbine[D]. Xi'an: Northwestern Polytechnical University, 2012. (in Chinese) 赵磊. 涡轮气动-声学一体化设计理论及方法研究[D]. 西安: 西北工业大学, 2012.[23] Goldstein M E. Aeroacoustics[M]. New York: McGraw-Hill International Book Co., 1976: 190-195.[24] Krejsa E A, Valerino M F. Interim prediction method for turbine noise, NASA-TM-X-73566[R]. Washington, D.C.: NASA, 1974.[25] Fisk W S. Supersonic transport noise reduction technology summary-phase 1, FAA-SS-1772-43[R]. Cincinnati: General Electric Co., 1972.[26] Sun X F, Hu Z A, Zhou S. Noise prediction of rotor-stator interaction for fan/compressor[J]. Acta Aeronautica et Astronautica Sinica, 1989, 10(1): 41-47. (in Chinese) 孙晓峰, 胡宗安, 周盛. 风扇/压气机转子、静子干涉噪声的预测方法[J]. 航空学报, 1989, 10(1): 41-47.[27] Pieter S, Jörgen Z. In-duct and far-field mode detection techniques[C]//13th AIAA/CEAS Aero-acoustics Conference, 2007.[28] Tyler J M, Sofrin T G. Axial flow compressor noise studies[J]. Transactions of the Society of Automotive Engineers, 1962, 70: 309-332. |