Stereo PIV Application to 6.5m x 5.5m Low-speed Wind Tunnel

External research report English OPEN
渡辺, 重哉; WATANABE, Shigeya; 加藤, 裕之; KATO, Hiroyuki;
  • Publisher: National Aerospace Laboratory(NAL)
  • Journal: National Aerospace Laboratory of Japan RESEARCH PROGRESS 200128-29 (issn: 1340-5977)
  • Publisher copyright policies & self-archiving
  • Subject: Stereo PIV, large-scale wind tunnel, subsonic flow

Large-scale wind tunnels at NAL have been utilized to acquire data on aerodynamic characteristics for the development of various types of airplane and aerospace vehicle. Although in most cases measurements concentrate on the information needed directly for vehicle desig... View more
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