Wind tunnel tests with approximately 2d flow were carried out for the RISOe- 1 airfoil in the VELUX open jet wind tunnel. The airfoil section was mounted in a test stand equipped with end plates to retain 2d flow conditions. The stand was then inserted into the tunnel test section. The ...
1) airfoil wind tunnel 翼型风洞1. The measurement and control of the model attitude angle in airfoil wind tunnel test; 翼型风洞实验模型姿态角的测量与控制更多例句>> 2) airfoil wind tunnel test 翼型风洞试验3) rotor model wind tunnel test 旋翼模型风洞试验...
3) wind-tunnel tests/wraparound-fin 风洞试验/卷弧翼4) airfoil wind tunnel 翼型风洞 1. The measurement and control of the model attitude angle in airfoil wind tunnel test; 翼型风洞实验模型姿态角的测量与控制 更多例句>> 5) wind tunnel test 模型风洞试验 1. The wind pressure distribution...
(1972): Wind Tunnel Tests of a Trapped Vortex-High Lift Airfoil. Advanced Technology Center Report No. ATC-B-94300/3TR-10, Dallas, TX. (Also available from U.S. NTIS; Document Number AD-762 077.)Wind Tunnel Tests of a Trapped Vortex-High Lift Airfoil. Krall, K. M,C. H. Haight....
Simulation of flow over double-element airfoil and wind tunnel test for use in vertical axis wind turbine 来自 掌桥科研 喜欢 0 阅读量: 82 作者:P Chougule,SRK Nielsen 摘要: Nowadays, small vertical axis wind turbines are receiving more attention due to their suitability in micro-electricity ...
摘要: PROBLEM TO BE SOLVED: To provide a method of wind tunnel test of airfoil which enables more accurate measurement of the aerodynamic properties of a 2-dimensional airfoil cross section.收藏 引用 批量引用 报错 分享 文库来源 其他来源 求助全文 METHOD OF WIND TUNNEL TEST OF AIRFOIL 优质文献...
DESIGN AND WIND TUNNEL TEST RESULTS OF A FLAPPED LAMINAR FLOW AIRFOIL FOR HIGH-PERFORMANCE SAILPLANE APPLICATIONS A laminar flow airfoil with camber changing flap, named DU89-1.34 / 74, has been designed and windtunnel tested for application in the high-performance sailplanes ASH-26E and ASW-...
Chinaa r t i c l ei n f oArticle history:Available online 23 May 2014Keywords:Wind turbineIcingBlade airfoilWind tunnel testIcing ratea b s t r a c tIcing on the blade surfaces of wind turbines is a serious problem in cold regions, which greatly affects theperformance of wind turbines...
Fig. 4.16 was constructed using wind tunnel tests in low-turbulence intensity flow for clean models at a Reynolds number of 1 × 106. The deep stall angle may be notably different in other flow conditions. Sign in to download full-size image Figure 4.14. The measured lift curve for an 18...
which are satisfied the main design requirements.From this study the NPU-WA airfoil data base including geometry and the wind tunnel test performance at Reynolds number from 1.0×106-5.0×106 are developed.The airfoils...