2-1 Wind Tunnel Rig for the Study of Roll Damping and Pitch Damping Effects of Free-Spinning Models at Supersonic Speed
21st:; International congress, Instrumentation in aerospace simulation facilities; ICIASF'05 record ; 2005 ; Sendai, Japan
2005-01-01
9 pages
IEEE cat no: 05CH37670
Aufsatz (Konferenz)
Englisch
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