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Filed under: Hovering- Motion effects on an IFR hovering task : analytical predictions and experimental results (National Aeronautics and Space Administration ;, 1971), by R. F. Ringland, Raymond E. Magdaleno, Robert L. Stapleford, Ames Research Center, and inc Systems Technology (page images at HathiTrust)
- Rapid-transition tests of a 1/4-scale model of the VZ-2 tilt-wing aircraft (National Aeronautics and Space Administration, 1961), by Louis P. Tosti, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 (National Aeronautics and Space Administration, 1960), by Joesph W. Jewel and Langley Research Center (page images at HathiTrust)
- Ground effect for lifting rotors in forward flight (National Aeronautics and Space Administration, 1960), by Harry H. Heyson and Langley Research Center (page images at HathiTrust)
- Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor (National Aeronautics and Space Administration, 1959), by John W. McKee and Langley Research Center (page images at HathiTrust)
- An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect (National Aeronautics and Space Administration, 1959), by Harry H. Heyson and Langley Research Center (page images at HathiTrust)
- Wind-tunnel and piloted flight simulator investigation of a deflected-slipstream VTOL airplane, the Ryan VZ-3RY (National Aeronautics and Space Administration, 1959), by Harry A. James and Ames Research Center (page images at HathiTrust)
- Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane (National Aeronautics and Space Administration, 1959), by David G. Koenig, Mark W. Kelly, Richard K. Greif, and Ames Research Center (page images at HathiTrust)
- Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight (National Aeronautics and Space Administration, 1962), by Kenneth W. Goodson, Kalman J. Grunwald, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Filed under: Helicopters -- HoveringFiled under: Rotors (Helicopters) -- HoveringFiled under: Rotor blades -- Hovering
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