中国航天
航天空气动力技术研究院
China Academy of Aerospace Aerodynamics (CAAA)

Transonic Wind Tunnel
  This is a sub-transonic wind tunnel of continuous type. The area of the test section is 0.76m×0.53m.Mach number ranges from 0.3 to 1.15. The quality of the flow field in this tunnel is of high uniformity, low turbulance and low noise.
·Force measurement and pressure measurement of vehicle models
·Flutter and buffeting test
·Test for interference between aeroplanes and missiles
·Hinge moment measurement
·Air inlet model test
·Dynamic derivative test
Visitor's Message
China Academy of Aerospace Aerodynamics
Address:17,Yun-gang West Road, Feng-tai District, Beijing
E-mail:caaa@bia701.com
Tel:(010)68743294 Fax:(010)68374758