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a.deg angle of attack angle positive direction closed lift-fan inlets Concluded configuration with 6L cruise configuration deflection angle positive deflection on longitudinal deg O Tail Effect of closed Effect of effective Effect of elevator Effect of ground Effect of tail effective velocity ratio elevator deflection Exit pressure ratio exits on longitudinal fan-exhaust deflection fan-exit fan-inlet mass flow Figure 17 Ground Effect ground proximity horizontal tail hover incidence on longitudinal inlets and exits it,deg o Tail landing configuration Langley Research Center Langley V/STOL tunnel Lift characteristics lift-cruise fans removed lift-fan VTOL transport longitudinal aerodynamic characteristics Mean geometric chord midspan NACA NASA TN Pitching-moment characteristics pods and lift-cruise ratio on longitudinal Spanwise location tail incidence thrust transition configuration 6L typical lift fan typical lift-cruise fan V/STOL Transport Model VTOL transition configuration Wind-Tunnel Investigation wingborne flight wingborne-flight configuration zero wind speed