AIAA-2003-6811 Analysis of the Twin-Fuselage Configuration and its H-Cabin Derivative
Annual technical forum; 3rd, Aviation technology integration and operations; ATIO 2003 ; 2003 ; Denver, CO
2003-01-01
10 pages
Aufsatz (Konferenz)
Englisch
aviation technology , integration , operations , aeronautics , ATIO , AIAA
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Twin-fuselage, twin rotor gyrodyne
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