[1] 王庆伟,刘波,侯为民,等.压气机转子叶片表面动态压力测量的探索[J].航空动力学报,2010,25(10):2327-2332.WANG Q W,LIU B,HOU W M,et al.Tentative research about pressure measurement on one point of compressor rotor blade surface[J].Journal of Aerospace Power,2010,25(10):2327-2332(in Chinese).
[2] WANG X,WANG X N,REN X,et al.Effects of tube system and data correction for fluctuating pressure test in wind tunnel[J].Chinese Journal of Aeronautics,2018,31(4):710-718.
[3] KUTIN J,SVETE A.On the theory of the frequency response of gas and liquid pressure measurement systems with connecting tubes[J].Measurement Science and Technology,2018,29:125108.
[4] 马宏伟,魏巍,张良,等.欠频响压力探针测量压气机动态流场的结果分析[J].航空发动机,2016,42(2):67-72.MA H W,WEI W,ZHANG L,et al.Analysis of measured unsteady flow field using a quasi fast response pressure probe[J].Aircraft Engine,2016,42(2):67-72(in Chinese).
[5] 李炜,邓勇生,赵中兵.固体火箭发动机用高频响压力传感器设计[J].固体火箭技术,2018,41(4):532-536.LI W,DENG Y S,ZHAO Z B.Design of high frequency pressure sensor for solid rocket motor[J].Solid Rocket Technology,2018,41(4):532-536(in Chinese).
[6] FAN L T,TO T C,HIRAOKA S,et al.Pressure fluctuations in a fluidized bed[J].Aiche Journal,1981,27(3):388-396.
[7] YATES J G,SIMONS S J R.Experimental methods in fluidization research[J].International Journal of Multiphase Flow,1994,20(8):297-330.
[8] ANTONINI C,PERSICO G,ROWE A L.Prediction of the dynamic response of complex transmission line systems for unsteady pressure measurements[J].Measurement Science and Technology,2008,19(12):125401.
[9] 柳兆荣,陈金娥,黄东群.压力传感器频率响应的分析[J].力学学报,1980,16(4):40-49.LIU Z R,CHEN J E,HUANG D Q.An analysis of frequency responses of pressure transducer[J].Journal of Mechanics,1980,16(4):40-49(in Chinese).
[10] 叶挺,梁庭,张文栋.压力测试中引压管的动态特性研究[J].中北大学学报(自然科学版),2011,32(2):222-226.YE T,LIANG T,ZHANG W D.Dynamic characteristic of transmission tube in pressure measurement system[J].Journal of North University of China(Natural Science Edition),2011,32(2):222-226(in Chinese).
[11] 黄俊钦.压力传感器动态数学模型研究[J].计量学报,1987,8(3):35-41.HUANG J Q.Research for dynamic mathematical model of pressure transducer[J].Acta Metrologica Sinica,1987,8(3):35-41(in Chinese).
[12] GOODSON R E,LEONARD R G.A survey of modeling techniques for fluid line transients[J].Journal of Basic Engineering,1972,94(2):474-482.
[13] IBERALL A S.Attenuation ofoscillatory pressures in instrument lines 1[J].Journal of Research of the National Bureau of Standards,1950,45(1):276-277.
[14] BERGH H,TIJDEMAN H.Theoretical and experimental results of dynamic response of pressure measuring system:NLR-TR F.238[R].Amsterdam:NLR,1965:1-19.
[15] RICHARDS W B.Propagation of sound waves in tubes of noncircular cross section NASA:NASA-TP-2601[R].Washington,D.C.:NASA,1986.
[16] 胡寿松.自动控制原理[M].4版.北京:科学出版社,2001:187-228.HU S S.Automatic control theory[M].4th ed.Beijing:Science Press,2001:187-228(in Chinese).
[17] 朱明武.动压测量[M].北京:国防工业出版社,1983:243-282.ZHU M W.Dynamic pressure measurement[M].Beijing:National Defense Industry Press,1983:243-282(in Chinese).
[18] SEMAAN R,SCHOLZ P.Pressure correction schemes and the use of the Wiener deconvolution method in pneumatic systems with short tubes[J].Experiments in Fluids,2012,53(3):829-837.
[19] ANDERSON R C,ENGLAND D V.Liquid-filled transient pressure measuring system:A method for determining frequency response:NASA TN D-6603[R].Washington,D.C.:NASA,1971.
[20] CHEN T S,LJUNG L.Implementation of algorithms for tuning parameters in regularized least squares problems in system identification[J].Automatica,2013,49(7):2213-2220.
[21] ISERMANN R.Practical aspects of process identification[J].Automatica,1980,16(5):575-587.
[22] VAN OMMEN J R,SCHOUTEN J C,VANDER STAPPEN M L M,et al.Response characteristics of probe-transducer systems for pressure measurements in gas-solid fluidized beds:How to prevent pitfalls in dynamic pressure measurements[J].Powder Technology,1999,113(1):199-218.
[23] KOBAYASHI H,LEGER T,WOLFF J M.Experimental and theoretical frequency response of pressure transducers for high speed turbomachinery[J].International Journal of Turbo & Jet-Engines,2000,17(2):153-160.
[24] PANTON R L,MILLER J M.Resonant frequencies of cylindrical Helmholtz resonators[J].The Journal of the Acoustica Society of America,1975,57(6):1533-1535.
[25] 王超,林大烜,丁红兵,等.基于凝结实验平台的音速喷嘴凝结现象研究[J].北京航空航天大学学报,2017,43(11):2232-2239.WANG C,LIN D X,DING H B,et al.Study on condensation in sonic nozzle based on experimental condensation apparatus[J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(11):2232-2239(in Chinese).
[26] WEGENER P P,CAGLIOSTRO D J.Periodic nozzle flow with heat addition[J].Combustion Science and Technology,1973,6(5):269-277. |