Aerodynamic characteristics of airship Zhiyuan-1

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• 作者：Ping Liu u (1)
  Gong-yi Fu (1)
  Li-jun Zhu ; /a> (1)
  Xiao-liang Wang A (2)
  
• 关键词：stratospheric airship ; hull configuration ; low ; speed wind tunnel test ; aerodynamic parameter ; pressure coefficient ; V 11
• 刊名：Journal of Shanghai Jiaotong University (Science)
• 出版年：2013
• 出版时间：December 2013
• 年：2013
• 卷：18
• 期：6
• 页码：679-687
• 全文大小：
• 作者单位：Ping Liu u (1)
  Gong-yi Fu (1)
  Li-jun Zhu ;/a> (1)
  Xiao-liang Wang A (2)
  
  1. School of Naval Architecture, Ocean and Civil Engineering, Shanghai Jiaotong University, Shanghai, 200240, China
  2. School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai, 200240, China
  
• ISSN：1995-8188

文摘

An airship named hiyuan-1was designed/fabricated/flied as a technical demonstration for stratospheric airship during 2007009 by Shanghai Jiaotong University. The calculation method and procedure of aerodynamic parameters were introduced, and the optimized configuration of the hull and the aerodynamic layout were given in this paper. Wind tunnel tests with different configurations, different pitch angles and different yaw angles were performed to study the wind load characteristics of the rigid model of the airship hiyuan-1in the 3.2 m wind tunnel at China Aerodynamics Research & Development Center. Also the numerical calculation about the test model was carried out to investigate the aerodynamic behavior. According to the results of wind test and numerical calculation, the excellent hull configuration of the airship hiyuan-1with lower drag characteristic was confirmed, which is based on optimism of the Michel transition law. And the phenomena of pressure coefficient distribution were discussed according to the results of wind tunnel test and numerical calculation at different flight attitudes.