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Large-scale wind tunnel investigation of a ducted fan - Deflected-slipstream model with an auxiliary wing

机译：管道风机的大型风洞调查 - 带辅助翼的偏转滑流模型

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摘要

Wind tunnel investigation of longitudinal aerodynamic characteristics of semispan wing deflected-slipstream configuration with double slotted flap and auxiliary wing

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作者
Falarski, M. D.; Mort, K. W.;
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年度 1971
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; SEMISPAN MODELS; SLIPSTREAMS; WIND TUNNEL STABILITY TESTS; AERODYNAMIC CONFIGURATIONS; DEFLECTION; WING SLOTS;

机译：空气动力学特征; sEmIspaN模型;滑流;风洞稳定性试验;空气动力学配置;偏转; WING sLOTs;

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专利

1. The experimental investigation of jet fan aerodynamics using wind tunnel modeling [J] . K. R. Mutama, A. E. Hall Journal of Fluids Engineering: Transactions of the ASME . 1996,第2期

机译：基于风洞模型的射流风机空气动力学实验研究
2. Experimental and Theoretical Flutter Investigation for a Range of Wing Wind-Tunnel Models [J] . Moradi Mehrdad, Sadeghi Morteza H., Dowell Earl H. Journal of Aircraft . 2018,第2期

机译：一系列机翼风洞模型的实验和理论颤振研究
3. Feasibility investigation of large-scale model suspended by cable-driven parallel robot in hypersonic wind tunnel test [J] . Wang Xiaoguang, Peng Miaojiao, Hu Zhenghong, Proceedings of the Institution of Mechanical Engineers . 2017,第G13期

机译：电缆并联机器人悬挂大型模型在高超音速风洞试验中的可行性研究
4. Wind Tunnel Test Results for a 600 mm Internal Diameter Merged Profile Annular Wing for a Ducted Fan Vehicle [C] . Miles Colman, Shinji Suzuki International powered lift conference . 2011

机译：风管车辆的600毫米内径合并轮廓环形翼的风洞测试结果
5. Wind tunnel investigation of jet fan aerodynamics. [D] . Mutama, Kuda Ronald. 1995

机译：射流风机空气动力学的风洞研究。
6. Airfoil Selection Procedure Wind Tunnel Experimentation and Implementation of 6DOF Modeling on a Flying Wing Micro Aerial Vehicle [O] . Taimur Ali Shams, Syed Irtiza Ali Shah, Ali Javed, 2020

机译：翼型微型飞行器的机翼选择程序风洞实验和6DOF建模实现
7. Flow field investigations on a wing installed Couter Rotating Ultra- high-bypass Fan engine simulator in the low speed wind tunnel DNW-LST [O] . Hegen G.H., Puffert-Meissner W., Dieterle L., 1999

机译：低速风洞DNW-LST中机翼安装的Couter旋转超高旁路风扇发动机模拟器的流场研究
8. Large-Scale Wind Tunnel Investigation of a Ducted Fan - Deflected-Slipstream Model with an Auxiliary Wing [R] . Falarski, M. D., Mort, K. W. 1971

机译：带辅助机翼的风管偏转滑流模型的大型风洞研究

Large-scale wind tunnel investigation of a ducted fan - Deflected-slipstream model with an auxiliary wing

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