CN112213069A - Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel - Google Patents
Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel Download PDFInfo
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- CN112213069A CN112213069A CN202011081758.4A CN202011081758A CN112213069A CN 112213069 A CN112213069 A CN 112213069A CN 202011081758 A CN202011081758 A CN 202011081758A CN 112213069 A CN112213069 A CN 112213069A
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- bent
- bent frame
- front edge
- test probe
- flow field
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
- G01M9/04—Details
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
- G01M9/065—Measuring arrangements specially adapted for aerodynamic testing dealing with flow
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- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
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CN202011081758.4A CN112213069B (en) | 2020-10-12 | 2020-10-12 | Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel |
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CN202011081758.4A CN112213069B (en) | 2020-10-12 | 2020-10-12 | Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel |
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CN112213069A true CN112213069A (en) | 2021-01-12 |
CN112213069B CN112213069B (en) | 2022-06-10 |
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CN202011081758.4A Active CN112213069B (en) | 2020-10-12 | 2020-10-12 | Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112985751A (en) * | 2021-02-01 | 2021-06-18 | 中国空气动力研究与发展中心超高速空气动力研究所 | Hypersonic wind tunnel stable section total temperature and total pressure test bent frame structure and manufacturing method |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040055374A1 (en) * | 2002-06-12 | 2004-03-25 | Cohen Adam J. | System and method for measuring the velocity of fluids |
US20110022040A1 (en) * | 2008-02-21 | 2011-01-27 | Erbe Elektromedizin Gmbh | Cryosurgical instrument |
US20170003152A1 (en) * | 2015-06-30 | 2017-01-05 | Commissariat A L'energie Atomique Et Aux Energies Al Ternatives | Miniature differential pressure flow sensor |
CN106482923A (en) * | 2016-10-28 | 2017-03-08 | 北京航天长征飞行器研究所 | Test device is demarcated in a kind of flow field being applied under hot environment |
CN107014582A (en) * | 2017-05-18 | 2017-08-04 | 西北工业大学 | A kind of stagnation temperature framed bent for continuous high-speed wind-tunnel hydrojet nitrogen cooling system |
KR101869648B1 (en) * | 2017-03-23 | 2018-06-21 | 국방과학연구소 | Flow rate calibration device for wind tunnel model and method thereof |
CN208156052U (en) * | 2018-05-21 | 2018-11-27 | 中国空气动力研究与发展中心超高速空气动力研究所 | A kind of electron number densitiy measurement two-probe arrangement |
CN208887888U (en) * | 2018-11-22 | 2019-05-21 | 中国空气动力研究与发展中心高速空气动力研究所 | Driving device is surveyed in supersonic wind tunnel flow field school |
CN110715789A (en) * | 2019-11-15 | 2020-01-21 | 中国空气动力研究与发展中心超高速空气动力研究所 | Water-cooling light-gathering optical fiber probe for hypersonic-velocity low-density wind tunnel stable section |
CN110823502A (en) * | 2019-11-20 | 2020-02-21 | 中国空气动力研究与发展中心超高速空气动力研究所 | Whole water-cooling bent in high temperature flow field |
-
2020
- 2020-10-12 CN CN202011081758.4A patent/CN112213069B/en active Active
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040055374A1 (en) * | 2002-06-12 | 2004-03-25 | Cohen Adam J. | System and method for measuring the velocity of fluids |
US20110022040A1 (en) * | 2008-02-21 | 2011-01-27 | Erbe Elektromedizin Gmbh | Cryosurgical instrument |
US20170003152A1 (en) * | 2015-06-30 | 2017-01-05 | Commissariat A L'energie Atomique Et Aux Energies Al Ternatives | Miniature differential pressure flow sensor |
CN106482923A (en) * | 2016-10-28 | 2017-03-08 | 北京航天长征飞行器研究所 | Test device is demarcated in a kind of flow field being applied under hot environment |
KR101869648B1 (en) * | 2017-03-23 | 2018-06-21 | 국방과학연구소 | Flow rate calibration device for wind tunnel model and method thereof |
CN107014582A (en) * | 2017-05-18 | 2017-08-04 | 西北工业大学 | A kind of stagnation temperature framed bent for continuous high-speed wind-tunnel hydrojet nitrogen cooling system |
CN208156052U (en) * | 2018-05-21 | 2018-11-27 | 中国空气动力研究与发展中心超高速空气动力研究所 | A kind of electron number densitiy measurement two-probe arrangement |
CN208887888U (en) * | 2018-11-22 | 2019-05-21 | 中国空气动力研究与发展中心高速空气动力研究所 | Driving device is surveyed in supersonic wind tunnel flow field school |
CN110715789A (en) * | 2019-11-15 | 2020-01-21 | 中国空气动力研究与发展中心超高速空气动力研究所 | Water-cooling light-gathering optical fiber probe for hypersonic-velocity low-density wind tunnel stable section |
CN110823502A (en) * | 2019-11-20 | 2020-02-21 | 中国空气动力研究与发展中心超高速空气动力研究所 | Whole water-cooling bent in high temperature flow field |
Non-Patent Citations (2)
Title |
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SUN QI等: ""Research on the design of the probe measuring the total pressure of exhaust of certain type of steam turbine"", 《PROCESS AUTOMATION INSTRUMENTATION》, vol. 36, no. 4, 20 April 2015 (2015-04-20), pages 56 - 9 * |
伍军等: "气体取样分析在脉冲燃烧风洞试验中的应用", 《空气动力学学报》, vol. 34, no. 03, 15 June 2016 (2016-06-15), pages 83 - 88 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112985751A (en) * | 2021-02-01 | 2021-06-18 | 中国空气动力研究与发展中心超高速空气动力研究所 | Hypersonic wind tunnel stable section total temperature and total pressure test bent frame structure and manufacturing method |
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CN112213069B (en) | 2022-06-10 |
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Inventor after: Zeng Lingguo Inventor after: Ren Hu Inventor after: Zhou Xin Inventor after: Wu Jinshui Inventor after: Wu Jun Inventor after: Li Xiangdong Inventor after: Bu Qing Qing Inventor after: Xing Yanchang Inventor after: Zhang Lin Inventor after: Pu Xuyang Inventor after: Li Hongbin Inventor before: Zeng Lingguo Inventor before: Wu Jun Inventor before: Li Xiangdong Inventor before: Bu Qing Qing Inventor before: Zhang Lin Inventor before: Pu Xuyang Inventor before: Li Hongbin Inventor before: Ren Hu Inventor before: Zhou Xin |
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