15-1 Stereoscopic PIV System Development for the JAXA 2m x 2m Transonic Wind Tunnel
21st:; International congress, Instrumentation in aerospace simulation facilities; ICIASF'05 record ; 2005 ; Sendai, Japan
01.01.2005
5 pages
IEEE cat no: 05CH37670
Aufsatz (Konferenz)
Englisch
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