Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage Bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors.
Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage Bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors
NACA -- Tech Note
1956
39 pages
Report
Englisch
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