Investigation to determine aerodynamic characteristics of aspect ratio 4 wing model with rotating fan to provide for VTOL and STOL capabilities; force, pressure, and power measurements obtained indicate significant loss in lift because of ground effects, improvement in aerodynamic characteristics and disk loading with duct inlet vanes, and possible propulsive force from duct exit vanes.
Wind-tunnel tests of semispan wing with fan rotating in plane of wing
NASA -- Tech Note
1959
44 pages
Report
English
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Computational Simulation of a Semispan Wing in a Wind Tunnel
British Library Conference Proceedings | 1998
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