Citation: | TANG J P,SHANG Y H,LI D,et al. Research on the double-inlet test method in low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, doi: 10.11729/syltlx20220059. |
[1] |
中国人民解放军总装备部军事训练教材编辑工作委员会. 低速风洞试验[M]. 北京: 国防工业出版社, 2002.
|
[2] |
SMITH A R, THORNE R, GOUTTENOIRE C, et al. Aerodynamic aspects of application of negative scarf intakes to high bypass ratio civil turbofans[C]//Proc of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2005: 4205. doi: 10.2514/6.2005-4205
|
[3] |
AREND D J, CASTNER R S, FRATE F C. A low cost, compact and versatile rig for integrated inlet and propulsion systems research[C]//Proc of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virginia: AIAA, 2006: 1313. doi: 10.2514/6.2006-1313
|
[4] |
CASTNER R S, SIMERLY S, RANKIN M. Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-foot by 6-foot supersonic wind tunnel[C]//Proc of the 2018 Applied Aerodynamics Conference. 2018: 2850. doi: 10.2514/6.2018-2850
|
[5] |
WOLTER J D. Multipurpose rotating rake arrays for integrated inlet and fan stage performance measurement[R]. National Aeronautics and Space Administration, GRC-E-DAA-TN47296, 2018.
|
[6] |
GUIMARÃES T, LOWE K T, O’BRIEN W F. Vortical flow development in round ducts across scales for engine inlet applications[J]. Experiments in Fluids, 2019, 60(4): 1–16. doi: 10.1007/s00348-019-2702-9[LinkOut
|
[7] |
高静, 郝卫东, 闫永昌, 等. 进气道低速特性试验技术研究[J]. 流体力学实验与测量, 2004, 18(1): 38–42. DOI: 10.3969/j.issn.1672-9897.2004.01.009
GAO J, HAO W D, YAN Y C, et al. Experimental investigation on low speed characteristics of inlet[J]. Experiments and Measurements in Fluid Mechanics, 2004, 18(1): 38–42. doi: 10.3969/j.issn.1672-9897.2004.01.009
|
[8] |
杨应凯. Bump进气道设计与试验研究[J]. 空气动力学学报, 2007, 25(3): 336–338,350. DOI: 10.3969/j.issn.0258-1825.2007.03.010
YANG Y K. The research of bump inlet design and test[J]. Acta Aerodynamica Sinica, 2007, 25(3): 336–338,350. doi: 10.3969/j.issn.0258-1825.2007.03.010
|
[9] |
巫朝君, 孔鹏, 王勋年, 等. 基于张线尾撑的进气道低速风洞试验技术研究[J]. 实验流体力学, 2012, 26(2): 86–89. DOI: 10.3969/j.issn.1672-9897.2012.02.019
WU C J, KONG P, WANG X N, et al. The investigation of the inlet test technology based on wire sting support in low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(2): 86–89. doi: 10.3969/j.issn.1672-9897.2012.02.019
|
[10] |
陈洪, 刘李涛, 巫朝君. 8 m × 6 m风洞大尺度模型进气道和喷流试验技术[J]. 空气动力学学报, 2017, 35(6): 875–878. DOI: 10.7638/kqdlxxb-2015.0133
CHEN H, LIU L T, WU C J. Inlet and jet test techniques for large scale model in 8 m × 6 m Low Speed Wind Tunnel[J]. Acta Aerodynamica Sinica, 2017, 35(6): 875–878. doi: 10.7638/kqdlxxb-2015.0133
|
[11] |
唐滨滨, 李长坤. 一种低速风洞大流量进气道试验系统研制[J]. 推进技术, 2018, 39(12): 2839–2844. DOI: 10.13675/j.cnki.tjjs.2018.12.024
TANG B B, LI C K. Development of a large mass flow inlet test system in low speed wind tunnel[J]. Journal of Propulsion Technology, 2018, 39(12): 2839–2844. doi: 10.13675/j.cnki.tjjs.2018.12.024
|
[12] |
巫朝君, 徐彬彬, 张为卓, 等. 低速风洞进气道试验柱形分布式引射器优化设计[J]. 航空动力学报, 2020, 35(12): 2482–2488. DOI: 10.13224/j.cnki.jasp.2020.12.002
WU C J, XU B B, ZHANG W Z, et al. Design and optimization of columniform distributed ejector for low speed wind tunnel inlet test[J]. Journal of Aerospace Power, 2020, 35(12): 2482–2488. doi: 10.13224/j.cnki.jasp.2020.12.002
|
[13] |
KOJIMA T, TANATSUGU N, SATO T, et al. Development study on axisymmetric air inlet for ATREX engine[C]//Proc of the 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. 2001: 1895. doi: 10.2514/6.2001-1895
|
[14] |
ALBERTSON C, EMAMI S, TREXLER C. Mach 4 test results of a dual-flowpath, turbine based combined cycle inlet[C]//Proc of the 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. 2006: 8138. doi: 10.2514/6.2006-8138
|
[15] |
CARTER M B, SHEA P R, FLAMM J D, et al. Experimental evaluation of inlet distortion on an ejector powered hybrid wing body at take-off and landing conditions (invited)[C]//Proc of the 54th AIAA Aerospace Sciences Meeting. 2016: 0010. doi: 10.2514/6.2016-0010
|
[16] |
欧平, 陈强, 田晓虎, 等. 双发进气道抽吸试验系统及流量高精度测量技术[J]. 空气动力学学报, 2016, 34(3): 392–397. DOI: 10.7638/kqdlxxb-2015.0118
OU P, CHEN Q, TIAN X H, et al. The pumping system and precise mass flow measuring technique for double-inlet wind tunnel test[J]. Acta Aerodynamica Sinica, 2016, 34(3): 392–397. doi: 10.7638/kqdlxxb-2015.0118
|