An Inviscid Model for Evaluating Wing Rock Suppression Methodologies
32nd Meeting, Aerospace sciences ; 1994 ; Reno; NV
1994-01-01
ALL
Separate papers nos AIAA 94-0047 - 94-0872 with gaps held only
Aufsatz (Konferenz)
Englisch
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An Inviscid Model for Evaluating Wing Rock Suppression Methodologies
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|Wing Rock Suppression Using Forebody Vortex Control
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