Use of wall suction in half model wind tunnel testing

机译：在半模型风洞测试中使用壁吸

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This is conference paper, presented at the 28th AIAA Applied Aerodynamics Conference: http://www.aiaa.org/

机译：这是会议论文，在第28届AIAA应用空气动力学会议上发表：http：//www.aiaa.org/

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Mailk Abdullah; Render Peter M.;
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年度 2010
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正文语种 en
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专利

1. Recent developments in the calculation of low-speed solid-walled wind tunnel wall interference in tests on large models Part Ⅰ: evaluation of three interference assessment methods [J] . J.E. Hackett Progress in Aerospace Sciences . 2003,第6a7期

机译：大型模型试验中低速实壁风洞墙干扰计算的最新进展第一部分：三种干扰评估方法的评估
2. Wind tunnel testing on a train model subjected to crosswinds with different windbreak walls [J] . Hashmi Syeda Anam, Hemida Hassan, Soper David Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2019,第期

机译：在火车模型的风洞测试与不同的风洞墙有交叉风
3. NUMERICAL INVESTIGATIONS OF THE INTERFERENCE EFFECT OF TRANSONIC WIND TUNNEL PERFORATED WALLS ON MODEL TEST RESULTS [J] . P.V. Savin TsAGI science journal . 2019,第5期

机译：跨音隧道穿孔壁对模型试验结果的干扰效应的数值研究
4. Use of Wall Suction In Half Model Wind Tunnel Testing [C] . A. Malik, P. Render AIAA Fluid Dynamics Conference and Exhibit;AIAA/ASME Joint Thermophysics and Heat Transfer Conference;AIAA CFD High-Lift Prediction Workshop;HILIFTPW-1;AIAA Aerodynamic Measurement Technology and Ground Testing Conference;AIAA Applied Aerodynamics Conference;Plasmadynamics and Lasers Conference;Flow Control Conference . 2010

机译：在半模型风洞测试中使用壁吸
5. Experimental investigation of slotted wall wind tunnel test sections for low interference road vehicle testing. [D] . Broughton, Cabot A. 1990

机译：用于低干扰道路车辆测试的开槽风洞测试段的实验研究。
6. Wind tunnel and numerical data on the ventilation performance of windcatcher with wing wall [O] . Payam Nejat, John Kaiser Calautit, Muhd Zaimi Abd. Majid, 2016

机译：风洞和带翼壁捕风器通风性能的数值数据
7. Suppression of junction flow effects in half model wind tunnel testing [O] . Malik Abdullah 2013

机译：在半模型风洞测试中抑制汇流效应
8. Reduction of Acoustic Disturbances in the Test Section of Supersonic Wind Tunnels by Laminarizing Their Nozzle and Test Section Wall Boundary Layers by Means of Suction [R] . Pfenninger, W., Syberg, J. 1974

机译：减少超音速风洞试验段中的声学干扰，通过吸力将其喷嘴和试验段壁边界层层压

Use of wall suction in half model wind tunnel testing

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