Citation: | Yu Tao, Wang Junpeng, Liu Xianghong, Zhao Jiaquan, Wu Jie. Measurements and data processing technology of freestream fluctuations in hypersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(5): 49-56. DOI: 10.11729/syltlx20180142 |
[1] |
伍荣林, 王振羽.风洞设计原理[M].北京:北京航空学院出版社, 1985.
Wu R L, Wang Z Y. Design principle of wind tunnel[M]. Beijing:Beijing Aviation Academy Press, 1985.
|
[2] |
Fedorov A. Transition and stability of high-speed boundary layers[J]. Annual Review of Fluid Mechanics, 2011, 43(1):79-95. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=7c2ca832ca33f26c09114620f4202345
|
[3] |
Schneider S P. Effects of high-speed tunnel noise on laminar-turbulent transition[J]. Journal of Spacecraft and Rockets, 2001, 38(3):323-333. DOI: 10.2514/2.3705
|
[4] |
Saric W S, Reed H L, Kerschen E J. Boundary-layer receptivity to freestream disturbances[J]. Annual Review of Fluid Mechanics, 2002, 34(1):291-319. http://d.old.wanfangdata.com.cn/OAPaper/oai_doaj-articles_1dde46788bca889843ee1299b85c6376
|
[5] |
刘向宏, 赖光伟, 吴杰.高超声速边界层转捩实验综述[J].空气动力学学报, 2018, 36(2):196-212. DOI: 10.7638/kqdlxxb-2018.0017
Liu X H, Lai G W, Wu J. Boundary-layer transition experi-ments in hypersonic flow[J]. Acta Aerodynamica Sinica, 2018, 36(2):196-212. DOI: 10.7638/kqdlxxb-2018.0017
|
[6] |
Yao Y F, Krishnan L, Sandham N D, et al. The effect of Mach number on unstable disturbances in shock/boundary-layer interactions[J]. Physics of Fluids, 2007, 19(5):054104. DOI: 10.1063/1.2720831
|
[7] |
Wieselsberger C. Der Luftwiderstand von Kugeln[J]. Zeitschrift für Flugtechnik und Motorluftschiffahrt, 1914, 5:140-145. http://cn.bing.com/academic/profile?id=3cb3844baa07361d329f52c1194a7667&encoded=0&v=paper_preview&mkt=zh-cn
|
[8] |
Zhong X L, Wang X W. Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers[J]. Annual Review of Fluid Mechanics, 2012, 44(1):527-561. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=e51c04f0fa97182358123d79cd7ba4ab
|
[9] |
Beckwith I E, Miller C G III. Aerothermodynamics and tran-sition in high-speed wind tunnels at NASA Langley[J]. Annual Review of Fluid Mechanics, 1990, 22(1):419-439. http://cn.bing.com/academic/profile?id=62af6597dc01a0219b5b723228387644&encoded=0&v=paper_preview&mkt=zh-cn
|
[10] |
Lei J, Zhong X L. Linear stability analysis of nose bluntness effects on hypersonic boundary layer transition[J]. Journal of Spacecraft and Rockets, 2012, 49(1):24-37. DOI: 10.2514/1.52616
|
[11] |
Kovasznay L S G. The hot-wire anemometer in supersonic flow[J]. Journal of the Aeronautical Sciences, 1950, 17(9):565-572. DOI: 10.2514/8.1725
|
[12] |
Kovasznay L S G. Turbulence in supersonic flow[J]. Journal of the Aeronautical Sciences, 1953, 20(10):657-674. DOI: 10.2514/8.2793
|
[13] |
Morkovin M V. On transition experiments at moderate super-sonic speeds[J]. Journal of the Aeronautical Sciences, 1957, 24(7):480-486. DOI: 10.2514/8.3887
|
[14] |
Morkovin M V. On supersonic wind tunnels with low free-stream disturbances[J]. Journal of Applied Mechanics, 1959, 26(3):319-323.
|
[15] |
Laufer J. Aerodynamic noise in supersonic wind tunnels[J]. Journal of the Aerospace Sciences, 1961, 28(9):685-692. DOI: 10.2514/8.9150
|
[16] |
Schneider S P. Development of hypersonic quiet tunnels[J]. Journal of Spacecraft and Rockets, 2008, 45(4):641-664. DOI: 10.2514/1.34489
|
[17] |
Spina E F, McGinley C B. Constant-temperature anemometry in hypersonic flow:critical issues and sample results[J]. Experiments in Fluids, 1994, 17(6):365-374. DOI: 10.1007/BF01877036
|
[18] |
Smits A J, Hayakawa K, Muck K C. Constant temperature hot-wire anemo-meter practice in supersonic flows[J]. Experiments in Fluids, 1984, 2(1):33-41. DOI: 10.1007/BF00266316
|
[19] |
Wu J, Radespiel R. Investigation of instability waves in a Mach 3 laminar boundary layer[J]. AIAA Journal, 2015, 53(12):3712-3725. DOI: 10.2514/1.J054040
|
[20] |
Weiss J, Knauss H, Wagner S, et al. Constant temperature hot-wire measurements in a short duration supersonic wind tunnel[J]. Aeronautical Journal, 2001, 105(1050):435-441. DOI: 10.1017/S0001924000012410
|
[21] |
Vrebalovich T. Application of hot-wire techniques in unsteady compressible flows[C]//Proc of ASME (1962) Symposium on Measurement of Unsteady Flow. 1962.
|
[22] |
Beckwith I E, Greel T R, Chen, F J, et al. Free stream noise and transition measurements in a Mach 3.5 pilot quiet tunnel[R]. AIAA-1983-42, 1983.
|
[23] |
Saric W S, Reed H L, Kerschen E J. Boundary-layer receptivity to freestream disturbances[J]. Annual Review of Fluid Mechanics, 2002, 34(1):291-319. http://d.old.wanfangdata.com.cn/OAPaper/oai_doaj-articles_1dde46788bca889843ee1299b85c6376
|
[24] |
Saric W S, Reed H L, White E B. Stability and transition of three-dimensional boundary layers[J]. Annual Review of Fluid Mechanics, 2003, 35(1):413-440. http://d.old.wanfangdata.com.cn/Periodical/yysxhlx-e201903009
|
[25] |
Schneider S P. Hypersonic laminar-turbulent transition on circular cones and scramjet forebodies[J]. Progress in Aerospace Sciences 2004, 40(1-2):1-50. DOI: 10.1016/j.paerosci.2003.11.001
|
[26] |
Logan P. Improved method of analyzing hot-wire measurements in supersonic turbulence[J]. AIAA Journal, 1989, 27(1):115-117. DOI: 10.2514/3.10104
|
[27] |
Logan P. Modal analysis of hot-wire measurements in super-sonic turbulence[R]. AIAA-1988-423, 1988.
|
[28] |
Masutti D, Spinosa E, Chazot O, et al. Disturbance level characterization of a hypersonic blowdown facility[J]. AIAA Journal, 2012, 50(12):2720-2730. DOI: 10.2514/1.J051502
|
[29] |
Wu J, Zamre P, Radespiel R. Flow quality experiment in a tandem nozzle wind tunnel at Mach 3[J]. Experiments in Fluids, 2015, 56(1):20. DOI: 10.1007/s00348-014-1887-1
|
[30] |
Wu J, Radespiel R. Damping insert materials for settling chambers of supersonic wind tunnels[J]. Experiments in Fluids, 2017, 58(3):19. DOI: 10.1007/s00348-017-2310-5
|
[31] |
Schilden T, Schröder W, Ali S R C, et al. Analysis of acoustic and entropy disturbances in a hypersonic wind tunnel[J]. Physics of Fluids, 2016, 28(5):056104. DOI: 10.1063/1.4948435
|
[32] |
Chaudhry R S, Candler G V. Computing measured spectra from hypersonic pitot probes with flow-parallel freestream distur-bances[J]. AIAA Journal, 2017, 55(12):1-12.
|
[33] |
Stainback P C, Wagner R D. A comparison of disturbance levels measured in hypersonic tunnels using a hot-wire anemometer and a pitot pressure probe[R]. AIAA-1972-1003, 1972.
|
[34] |
Zhang C H, Tang Q, Lee C B. Hypersonic boundary-layer transition on a flared cone[J]. Acta Mechanica Sinica, 2013, 29(1):48-54. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201802002
|
[35] |
Wu J, Radespiel R. Experimental investigation of a newly designed supersonic wind tunnel[J]. Progress in Flight Physics, 2015(7):123-147.
|
[36] |
Wu J. Boundary-layer instability experiments in a tandem nozzle supersonic wind tunnel[M]. Germany:ShakerVerlag GmbH, 2015.
|
[37] |
Wu J, Liu X J, Radespiel R. RANS simulations of a tandem nozzle supersonic wind tunnel[J]. Aerospace Science and Technology, 2015, 49:215-224. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=c71a696891579b3b4bf8927039b0cfab
|
[38] |
Wu J, Radespiel R. Tandem nozzle supersonic wind tunnel design[J]. International Journal of Engineering Systems Modelling and Simulation, 2013, 5(1):8-18. http://d.old.wanfangdata.com.cn/NSTLQK/NSTL_QKJJ0229412597/
|
[39] |
Wu J, Radespiel R. Damping insert materials for settling chambers of supersonic wind tunnels[J]. Experiments in Fluids, 2017, 58(3):19. DOI: 10.1007/s00348-017-2310-5
|
[40] |
吴杰. Ludwieg管向超声速流域拓展的设计技术[J].空气动力学学报, 2018, 36(3):480-492. DOI: 10.7638/kqdlxxb-2017.0042
Wu J. Extention of hypersonic Ludwieg tube to supersonic wind tunnel[J]. Acta Aerodynamica Sinica, 2018, 36(3):480-492. DOI: 10.7638/kqdlxxb-2017.0042
|
[41] |
Stephan S, Wu J, Radespiel R. Propulsive jet influence on generic launcher base flow[J]. CEAS Space Journal, 2015, 7(4):453-473. DOI: 10.1007/s12567-015-0098-9
|
[42] |
Laufer J, McClellan R. Measurements of heat transfer from fine wires in supersonic flows[J]. Journal of Fluid Mechanics, 1956, 1(3):276-289. DOI: 10.1017/S0022112056000160
|
[43] |
Beckwith I E. Comments on settling chamber design for quiet, blowdown wind tunnels[R]. NASA-TM-81948, 1981.
|
[44] |
Duan L, Choudhari M M, Chou A, et al. Characterization of freestream disturbances in conventional hypersonic wind tunnels[R]. AIAA-2018-0347, 2018.
|
[45] |
Ali S R C, Wu J, Radespiel R, et al. High-frequency measure-ments of acoustic and entropy disturbances in a hypersonic wind tunnel[R]. AIAA-2014-2644, 2014.
|
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