Longitudinal Aerodynamic Characteristics of a Deflected-thrust Propulsive-lift Transport Model |
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28 32 Spanwise 32 20 Spanwise 32 Spanwise location 97 Open angle at horizontal-tail angle of attack attack on downwash Closed 0 Open Closed 97 coefficient on longitudinal Concluded Continued cowl assemblies Cruise configuration Cụ Cụ Cụ deg CD Figure deg Figure downwash angle Effect of angle Effect of tail Effect of thrust engine 10-45 engine externally blown flap Figure 58 Figure 66 horizontal tail horizontal-tail location i+,deg Inlet Tail i+,deg Tail incidence on longitudinal Inlet Open Tail inlets closed inlets open 75-45 inlets open Cụ Landing configuration Langley V/STOL tunnel longitudinal aerodynamic characteristics Mean geometric chord NASA TN Open 0 Closed Open 0 Open Open 1.99 Open Open 2.00 Open Open 24 Open 5 Open Open Open static-thrust STOL tail and horizontal tail incidence Tail off Closed Tail off Open Take-off configuration thrust coefficient vertical tail Wind-Tunnel Investigation Wing Сн